CROSS-REFERENCE TO RELATED APPLICATIONS The present application claims the benefit of U.S. Provisional Application No. 60/610,509 filed on Sep. 16, 2004, and U.S. Provisional Application No. 60/590,894 filed on Jul. 23, 2004, both of which are incorporated herein by reference in their entireties.
TECHNICAL FIELD This invention relates generally to radiation therapy systems, and more particularly to systems and methods for accurately locating and tracking a target in real time for guiding and assessing radiation therapy. The invention, however, is also useful in other medical applications.
BACKGROUND OF THE INVENTION Radiation therapy has become a significant and highly successful process for treating prostate cancer, lung cancer, brain cancer and many other types of localized cancers. Radiation therapy procedures generally involve (a) planning processes to determine the parameters of the radiation (e.g., dose, shape, etc.), (b) patient setup processes to position the target at a desired location relative to the radiation beam, (c) radiation sessions to irradiate the cancer, and (d) verification processes to assess the efficacy of the radiation sessions. Many radiation therapy procedures require several radiation sessions (i.e., radiation fractions) over a period of approximately 5-45 days.
To improve the treatment of localized cancers with radiotherapy, it is generally desirable to increase the radiation dose because higher doses are more effective at destroying most cancers. Increasing the radiation dose, however, also increases the potential for complications to healthy tissues. The efficacy of radiation therapy accordingly depends on both the total dose of radiation delivered to the tumor and the dose of radiation delivered to normal tissue adjacent to the tumor. To protect the normal tissue adjacent to the tumor, the radiation should be prescribed to a tight treatment margin around the target such that only a small volume of healthy tissue is irradiated. For example, the treatment margin for prostate cancer should be selected to avoid irradiating rectal, bladder and bulbar urethral tissues. Similarly, the treatment margin for lung cancer should be selected to avoid irradiating healthy lung tissue or other tissue. Therefore, it is not only desirable to increase the radiation dose delivered to the tumor, but it also desirable to mitigate irradiating healthy tissue.
One difficulty of radiation therapy is that the target often moves within the patient either during or between radiation sessions. For example, the prostate gland moves within the patient during radiation treatment sessions because of respiration motion and/or organ filling/emptying (e.g., full or empty bladder). Tumors in the lungs also move during radiation sessions because of respiration motion and cardiac functions (e.g., heartbeats and vasculature constriction/expansion). To compensate for such movement, the treatment margins are generally larger than desired so that the tumor does not move out of the treatment volume. This is not a desirable solution because the larger treatment margins may irradiate a larger volume of normal tissue.
Another challenge in radiation therapy is accurately aligning the tumor with the radiation beam. Current setup procedures generally align external reference markings on the patient with visual alignment guides for the radiation delivery device. For an example, a tumor is first identified within the patient using an imaging system (e.g., X-ray, computerized tomography (CT), magnetic resonance imaging (MRI), or ultrasound system). The approximate location of the tumor relative to two or more alignment points on the exterior of the patient is then determined. During setup, the external marks are aligned with a reference frame of the radiation delivery device to position the treatment target within the patient at the beam isocenter of the radiation beam (also referenced herein as the machine isocenter). Conventional setup procedures using external marks are generally inadequate because the target may move relative to the external marks between the patient planning procedure and the treatment session and/or during the treatment session. As such, the target may be offset from the machine isocenter even when the external marks are at their predetermined locations for positioning the target at the machine isocenter. Reducing or eliminating such an offset is desirable because any initial misalignment between the target and the radiation beam will likely cause normal tissue to be irradiated. Moreover, if the target moves during treatment because of respiration, organ filling, or cardiac conditions, any initial misalignment will likely further exacerbate irradiation of normal tissue. Thus, the day-by-day and moment-by-moment changes in target motion have posed significant challenges for increasing the radiation dose applied to patients.
Conventional setup and treatment procedures using external marks also require a direct line-of-sight between the marks and a detector. This requirement renders these systems useless for implanted markers or markers that are otherwise in the patient (i.e., out of the line-of-sight of the detector and/or the light source). Thus, conventional optical tracking systems have many restrictions that limit their utility in medical applications.
BRIEF DESCRIPTION OF THE DRAWINGSFIG. 1 is a side elevation view of a tracking system for use in localizing and monitoring a target in accordance with an embodiment of the present invention. Excitable markers are shown implanted in or adjacent to a target in the patient.
FIG. 2 is a schematic elevation view of the patient on a movable support table and of markers implanted in the patient.
FIG. 3 is a side view schematically illustrating a localization system and a plurality of markers implanted in a patient in accordance with an embodiment of the invention.
FIG. 4 is a flow diagram of an integrated radiation therapy process that uses real time target tracking for radiation therapy in accordance with an embodiment of the invention.
FIG. 5A is a representation of a CT image illustrating an aspect of a system and method for real time tracking of targets in radiation therapy and other medical applications.
FIG. 5B is a diagram schematically illustrating a reference frame of a CT scanner.
FIG. 6 is a screenshot of a user interface for displaying an objective output in accordance with an embodiment of the invention.
FIG. 7 is an isometric view of a radiation session in accordance with an embodiment of the invention.
FIG. 8A is an isometric view of a marker for use with a localization system in accordance with an embodiment of the invention.
FIG. 8B is a cross-sectional view of the marker ofFIG. 8A taken along line8B-8B.
FIG. 8C is an illustration of a radiographic image of the marker ofFIGS. 8A-8B.
FIG. 9A is an isometric view of a marker for use with a localization system in accordance with another embodiment of the invention.
FIG. 9B is a cross-sectional view of the marker ofFIG. 9A taken alongline9B-9B.
FIG. 10A is an isometric view of a marker for use with a localization system in accordance with another embodiment of the invention.
FIG. 10B is a cross-sectional view of the marker ofFIG. 10A taken alongline10B-10B.
FIG. 11 is an isometric view of a marker for use with a localization system in accordance with another embodiment of the invention.
FIG. 12 is an isometric view of a marker for use with a localization system in accordance with yet another embodiment of the invention.
FIG. 13 is a schematic block diagram of a localization system for use in tracking a target in accordance with an embodiment of the invention.
FIG. 14 is a schematic view of an array of coplanar source coils carrying electrical signals in a first combination of phases to generate a first excitation field.
FIG. 15 is a schematic view of an array of coplanar source coils carrying electrical signals in a second combination of phases to generate a second excitation field.
FIG. 16 is a schematic view of an array of coplanar source coils carrying electrical signals in a third combination of phases to generate a third excitation field.
FIG. 17 is a schematic view of an array of coplanar source coils illustrating a magnetic excitation field for energizing markers in a first spatial orientation.
FIG. 18 is a schematic view of an array of coplanar source coils illustrating a magnetic excitation field for energizing markers in a second spatial orientation.
FIG. 19A is an exploded isometric view showing individual components of a sensor assembly for use with a localization system in accordance with an embodiment of the invention.
FIG. 19B is a top plan view of a sensing unit for use in the sensor assembly ofFIG. 19A.
FIG. 20 is a schematic diagram of a preamplifier for use with the sensor assembly ofFIG. 19A.
FIG. 21 is a graph of illustrative tumor motion ellipses from experimental phantom based studies of the system.
FIG. 22 is a graph of root mean square (RMS) error from experimental phantom based studies of the system.
FIG. 23 is an exemplary histogram of localization error from experimental phantom based studies of the system.
FIG. 24 is graph of position error as a function of speed from experimental phantom based studies of the system.
In the drawings, identical reference numbers identify similar elements or components. The sizes and relative positions of elements in the drawings are not necessarily drawn to scale. For example, the shapes of various elements and angles are not drawn to scale, and some of these elements are arbitrarily enlarged and positioned to improve drawing legibility. Further, the particular shapes of the elements as drawn, are not intended to convey any information regarding the actual shape of the particular elements, and have been solely selected for ease of recognition in the drawings.
DETAILED DESCRIPTION In the following description, certain specific details are set forth in order to provide a thorough understanding of various embodiments of the invention. However, one skilled in the relevant art will recognize that the invention may be practiced without one or more of these specific details, or with other methods, components, materials, etc. In other instances, well-known structures associated with target locating and tracking systems have not been shown or described in detail to avoid unnecessarily obscuring descriptions of the embodiments of the invention.
Unless the context requires otherwise, throughout the specification and claims which follow, the word “comprise” and variations thereof, such as, “comprises” and “comprising” are to be construed in an open, inclusive sense that is as “including, but not limited to.”
Reference throughout this specification to “one embodiment” or “an embodiment” means that a particular feature, structure or characteristic described in connection with the embodiment is included in at least one embodiment of the present invention. Thus, the appearances of the phrases “in one embodiment” or “in an embodiment” in various places throughout this specification are not necessarily all referring to the same embodiment. Further more, the particular features, structures, or characteristics may be combined in any suitable manner in one or more embodiments.
The headings provided herein are for convenience only and do not interpret the scope or meaning of the claimed invention.
A. Overview
FIGS. 1-24 illustrate a system and several components for locating, tracking and monitoring a target within a patient in real time in accordance with embodiments of the present invention. The system and components guide and control the radiation therapy to more effectively treat the target. Several embodiments of the systems described below with reference toFIGS. 1-24 can be used to treat targets in the lung, prostate, head, neck, breast and other parts of the body in accordance with aspects of the present invention. Additionally, the markers and localization systems shown inFIGS. 1-24 may also be used in surgical applications or other medical applications. Like reference numbers refer to like components and features throughout the various figures.
Several embodiments of the invention are directed towards methods for tracking a target, i.e., measuring the position and/or the rotation of a target in substantially real time, in a patient in medical applications. One embodiment of such a method comprises collecting position data of a marker that is substantially fixed relative to the target. This embodiment further includes determining the location of the marker in an external reference frame (i.e., a reference frame outside the patient) and providing an objective output in the external reference frame that is responsive to the location of the marker. The objective output is repeatedly provided at a frequency/periodicity that adequately tracks the location of the target in real time within a clinically acceptable tracking error range. As such, the method for tracking the target enables accurate tracking of the target during diagnostic, planning, treatment or other types of medical procedures. In many specific applications, the objective output is provided within a suitably short latency after collecting the position data and at a sufficiently high frequency to use the data for such medical procedures.
Another specific embodiment is a method for treating a target in a patient with an ionizing radiation beam that includes collecting position information of a marker implanted within a patient at a site relative to the target at a time tn, and providing an objective output indicative of the location of the target based on the position information collected at time tn. The objective output is provided to a memory device, user interface, and/or radiation delivery machine within 2 seconds or less of the time tnwhen the position information was collected. This embodiment of the method can further include providing the objective output at a periodicity of 2 seconds or less during at least a portion of a treatment procedure. For example, the method can further include generating a beam of ionizing radiation and directing the beam to a machine isocenter, and continuously repeating the collecting procedure and the providing procedure every 10-200 ms while irradiating the patient with the ionizing radiation beam.
Another embodiment of a method for tracking a target in a patient includes obtaining position information of a marker situated within the patient at a site relative to the target, and determining a location of the marker in an external reference frame based on the position information. This embodiment further includes providing an objective output indicative of the location of the target to a user interface at (a) a sufficiently high frequency so that pauses in representations of the target location at the user interface are not readily discernable by a human, and (b) a sufficiently low latency to be at least substantially contemporaneous with obtaining the position information of the marker.
Another embodiment of the invention is directed toward a method of treating a target of a patient with an ionizing radiation beam by generating a beam of ionizing radiation and directing the beam relative to the target. This method further includes collecting position information of a marker implanted within the patient at a site relative to the target while directing the beam toward the beam isocenter. Additionally, this method includes providing an objective output indicative of a location of the target relative to the beam isocenter based on the collected position information. This method can further include correlating the objective output with a parameter of the beam, and controlling the beam based upon the objective output. For example, the beam can be gated to only irradiate the patient when the target is within a desired irradiation zone. Additionally, the patient can be moved automatically and/or the beam can be shaped automatically according to the objective output to provide dynamic control in real time that maintains the target at a desired position relative to the beam isocenter while irradiating the patient.
Various embodiments of the invention are described in this section to provide specific details for a thorough understanding and enabling description of these embodiments. A person skilled in the art, however, will understand that the invention may be practiced without several of these details, or that additional details can be added to the invention. Where the context permits, singular or plural terms may also include the plural or singular term, respectively. Moreover, unless the word “or” is expressly limited to mean only a single item exclusive from the other items in reference to a list of at least two items, then the use of “or” in such a list is to be interpreted as including (a) any single item in the list, (b) all of the items in the list, or (c) any combination of items in the list. Additionally, the term “comprising” is used throughout to mean including at least the recited feature(s) such that any greater number of the same feature and/or types of other features or components are not precluded.
B. Radiation Therapy Systems with Real Time Tracking Systems
FIGS. 1 and 2 illustrate various aspects of aradiation therapy system1 for applying guided radiation therapy to a target2 (e.g., a tumor) within alung4, prostate, breast, head, neck or other part of apatient6. Theradiation therapy system1 has alocalization system10 and aradiation delivery device20. Thelocalization system10 is a tracking unit that locates and tracks the actual position of thetarget2 in real time during treatment planning, patient setup, and/or while applying ionizing radiation to the target from the radiation delivery device. Thus, although thetarget2 may move within the patient because of breathing, organ filling/emptying, cardiac functions or other internal movement as described above, thelocalization system10 accurately tracks the motion of the target relative to the external reference frame of the radiation delivery device or other external reference frame outside of the patient to accurately deliver radiation within a small margin around the target. Thelocalization system10 can also monitor the configuration and trajectory of the marker to provide an early indicator of a change in the tumor without using ionizing radiation. Moreover, thelocalization system10 continuously tracks the target and provides objective data (e.g., three-dimensional coordinates in an absolute reference frame) to a memory device, user interface, linear accelerator, and/or other device. Thesystem1 is described below in the context of guided radiation therapy for treating a tumor or other target in the lung of the patient, but the system can be used for tracking and monitoring the prostate gland or other targets within the patient for other therapeutic and/or diagnostic purposes.
The radiation delivery source of the illustrated embodiment is an ionizing radiation device20 (i.e., a linear accelerator). Suitable linear accelerators are manufactured by Varian Medical Systems, Inc. of Palo Alto, Calif.; Siemens Medical Systems, Inc. of Iselin, N.J.; Elekta Instruments, Inc. of Iselin, N.J.; or Mitsubishi Denki Kabushik Kaisha of Japan. Such linear accelerators can deliver conventional single or multi-field radiation therapy, 3D conformal radiation therapy (3D CRT), intensity modulated radiation therapy (IMRT), stereotactic radiotherapy, and tomo therapy. Theradiation delivery source20 can deliver a gated, contoured or shapedbeam21 of ionizing radiation from amovable gantry22 to an area or volume at a known location in an external, absolute reference frame relative to theradiation delivery source20. The point or volume to which theionizing radiation beam21 is directed is referred to as the machine isocenter.
The tracking system includes thelocalization system10 and one ormore markers40. Thelocalization system10 determines the actual location of themarkers40 in a three-dimensional reference frame, and themarkers40 are typically implanted within thepatient6. In the embodiment illustrated inFIGS. 1 and 2, more specifically, three markers identified individually asmarkers40a-care implanted in or near thelung4 of thepatient6 at locations in or near thetarget2. In other applications, a single marker, two markers, or more than three markers can be used depending upon the particular application. Two markers, for example, are desirable because the location of the target can be determined accurately, and also because any relative displacement between the two markers over time can be used to monitor marker migration in the patient. Themarkers40 are desirably placed relative to thetarget2 such that themarkers40 are at least substantially fixed relative to the target2 (e.g., the markers move directly with the target or at least in direct proportion to the movement of the target). The relative positions between themarkers40 and the relative positions between a target isocenter T of thetarget2 and themarkers40 can be determined with respect to an external reference frame defined by a CT scanner or other type of imaging system during a treatment planning stage before the patient is placed on the table. In the particular embodiment of thesystem1 illustrated inFIGS. 1 and 2, thelocalization system10 tracks the three-dimensional coordinates of themarkers40 in real time relative to an absolute external reference frame during the patient setup process and while irradiating the patient to mitigate collateral effects on adjacent healthy tissue and to ensure that the desired dosage is applied to the target.
C. General Aspects of Markers and Localization Systems
FIG. 3 is a schematic view illustrating the operation of an embodiment of thelocalization system10 andmarkers40a-cfor treating a tumor or other target in the patient. Thelocalization system10 and themarkers40a-care used to determine the location of the target2 (FIGS. 1 and 2) before, during and after radiation sessions. More specifically, thelocalization system10 determines the locations of themarkers40a-cand provides objective target position data to a memory, user interface, linear accelerator and/or other device in real time during setup, treatment, deployment, simulation, surgery, and/or other medical procedures. In one embodiment of the localization system, real time means that indicia of objective coordinates are provided to a user interface at (a) a sufficiently high refresh rate (i.e., frequency) such that pauses in the data are not humanly discernable and (b) a sufficiently low latency to be at least substantially contemporaneous with the measurement of the location signal. In other embodiments, real time is defined by higher frequency ranges and lower latency ranges for providing the objective data to a radiation delivery device, or in still other embodiments real time is defined as providing objective data responsive to the location of the markers (e.g., at a frequency that adequately tracks the location of the target in real time and/or a latency that is substantially contemporaneous with obtaining position data of the markers).
1. Localization Systems
Thelocalization system10 includes an excitation source60 (e.g., a pulsed magnetic field generator), asensor assembly70, and acontroller80 coupled to both theexcitation source60 and thesensor assembly70. Theexcitation source60 generates an excitation energy to energize at least one of themarkers40a-cin the patient6 (FIG. 1). The embodiment of theexcitation source60 shown inFIG. 3 produces a pulsed magnetic field at different frequencies. For example, theexcitation source60 can frequency multiplex the magnetic field at a first frequency E1to energize thefirst marker40a, a second frequency E2to energize thesecond marker40b, and a third frequency E3to energize thethird marker40c. In response to the excitation energy, themarkers40a-cgenerate location signal L1-3at unique response frequencies. More specifically, thefirst marker40agenerates a first location signal L1at a first frequency in response to the excitation energy at the first frequency E1, thesecond marker40bgenerates a second location signal L2at a second frequency in response to the excitation energy at the second frequency E2, and thethird marker40cgenerates a third location signal L3at a third frequency in response to the excitation energy at the third frequency E3. In an alternative embodiment with two markers, the excitation source generates the magnetic field at frequencies E1and E2, and themarkets40a-bgenerate location signals L1and L2, respectively.
Thesensor assembly70 can include a plurality of coils to sense the location signals L1-3from themarkers40a-c. Thesensor assembly70 can be a flat panel having a plurality of coils that are at least substantially coplanar relative to each other. In other embodiments, thesensor assembly70 may be a non-planar array of coils.
Thecontroller80 includes hardware, software or other computer-operable media containing instructions that operate theexcitation source60 to multiplex the excitation energy at the different frequencies E1-3. For example, thecontroller80 causes theexcitation source60 to generate the excitation energy at the first frequency E1for a first excitation period, and then thecontroller80 causes theexcitation source60 to terminate the excitation energy at the first frequency E1for a first sensing phase during which thesensor assembly70 senses the first location signal L1from thefirst marker40awithout the presence of the excitation energy at the first frequency E1. Thecontroller80 then causes theexcitation source60 to: (a) generate the second excitation energy at the second frequency E2for a second excitation period; and (b) terminate the excitation energy at the second frequency E2for a second sensing phase during which thesensor assembly70 senses the second location signal L2from thesecond marker40bwithout the presence of the second excitation energy at the second frequency E2. Thecontroller80 then repeats this operation with the third excitation energy at the third frequency E3such that thethird marker40ctransmits the third location signal L3to thesensor assembly70 during a third sensing phase. As such, theexcitation source60 wirelessly transmits the excitation energy in the form of pulsed magnetic fields at the resonant frequencies of themarkers40a-cduring excitation periods, and themarkers40a-cwirelessly transmit the location signals L1-3to thesensor assembly70 during sensing phases. It will be appreciated that the excitation and sensing phases can be repeated to permit averaging of the sensed signals to reduce noise.
The computer-operable media in thecontroller80, or in a separate signal processor, or other computer also includes instructions to determine the absolute positions of each of themarkers40a-cin a three-dimensional reference frame. Based on signals provided by thesensor assembly70 that correspond to the magnitude of each of the location signals L1-3, thecontroller80 and/or a separate signal processor calculates the absolute coordinates of each of themarkers40a-cin the three-dimensional reference frame. The absolute coordinates of themarkers40a-care objective data that can be used to calculate the coordinates of the target in the reference frame. When multiple markers are used, the rotation of the target can also be calculated.
2. Real Time Tracking
Thelocalization system10 and at least one of amarker40 enables real time tracking of thetarget2 relative to the machine isocenter or another external reference frame outside of the patient during treatment planning, set up, radiation sessions, and at other times of the radiation therapy process. In many embodiments, real time tracking means collecting position data of the markers, determining the locations of the markers in an external reference frame, and providing an objective output in the external reference frame that is responsive to the location of the markers. The objective output is provided at a frequency that adequately tracks the target in real time and/or a latency that is at least substantially contemporaneous with collecting the position data (e.g., within a generally concurrent period of time).
For example, several embodiments of real time tracking are defined as determining the locations of the markers and calculating the location of the target relative to the machine isocenter at (a) a sufficiently high frequency so that pauses in representations of the target location at a user interface do not interrupt the procedure or are readily discernable by a human, and (b) a sufficiently low latency to be at least substantially contemporaneous with the measurement of the location signals from the markers. Alternatively, real time means that thelocation system10 calculates the absolute position of eachindividual marker40 and/or the location of the target at a periodicity of 1 ms to 5 seconds, or in many applications at a periodicity of approximately 10-100 ms, or in some specific applications at a periodicity of approximately 20-50 ms. In applications for user interfaces, for example, the periodicity can be 12.5 ms (i.e., a frequency of 80 Hz), 16.667 ms (60 Hz), 20 ms (50 Hz), and/or 50 ms (20 Hz).
Alternatively, real time tracking can further mean that thelocation system10 provides the absolute locations of themarkers40 and/or thetarget2 to a memory device, user interface, linear accelerator or other device within a latency of 10 ms to 5 seconds from the time the localization signals were transmitted from themarkers40. In more specific applications, the location system generally provides the locations of themarkers40 and/ortarget2 within a latency of about 20-50 ms. Thelocation system10 accordingly provides real time tracking to monitor the position of themarkers40 and/or thetarget2 with respect to an external reference frame in a manner that is expected to enhance the efficacy of radiation therapy because higher radiation doses can be applied to the target and collateral effects to healthy tissue can be mitigated.
Alternatively, real-time tracking can further be defined by the tracking error. Measurements of the position of a moving target are subject to motion-induced error, generally referred to as a tracking error. According to aspects of the present invention, thelocalization system10 and at least onemarker4 enable real time tracking of thetarget2 relative to the machine isocenter or another external reference frame with a tracking error that is within clinically meaningful limits.
Tracking errors are due to two limitations exhibited by any practical measurement system, specifically (a) latency between the time the target position is sensed and the time the position measurement is made available, and (b) sampling delay due to the periodicity of measurements. For example, if a target is moving at 5 cm/s and a measurement system has a latency of 200 ms, then position measurements will be in error by 1 cm. The error in this example is due to latency alone, independent of any other measurement errors, and is simply due to the fact that the target has moved between the time its position is sensed and the time the position measurement is made available for use. If this exemplary measurement system further has a sampling periodicity of 200 ms (i.e., a sampling frequency of 5 Hz), then the peak tracking error increases to 2 cm, with an average tracking error of 1.5 cm.
For a real time tracking system to be useful in medical applications, it is desirable to keep the tracking error within clinically meaningful limits. For example, in a system for tracking motion of a tumor in a lung for radiation therapy, it may be desirable to keep the tracking error within 5 mm. Acceptable tracking errors may be smaller when tracking other organs for radiation therapy. In accordance with aspects of the present invention, real time tracking refers to measurement of target position and/or rotation with tracking errors that are within clinically meaningful limits.
The system described herein uses one or more markers to serve as registration points to characterize target location, rotation, and motion. In accordance with aspects of the invention, the markers have a substantially fixed relationship with the target. If the markers did not have a substantially fixed relationship with the target another type of tracking error would be incurred. This generally requires the markers to be fixed or implanted sufficiently close to the target in order that tracking errors be within clinically meaningful limits, thus, the markers may be placed in tissue or bone that exhibits representative motion of the target. For example, with respect to the prostate, tissue that is representative of the target's motion would include tissue in close proximity or adjacent to the prostate. Tissue adjacent to a target involving the prostate may include the prostate gland, the tumor itself, or tissue within a specified radial distance from the target. With respect to the prostate, tracking tissue that is a 5 cm radial distance from the target would provide representative motion that is clinically useful to the motion of the target. In accordance with alternative target tracking locations, the radial distance may be greater or lesser.
According to aspects of the present invention, the marker motion is a surrogate for the motion of the target. Accordingly, the marker is placed such that it moves in direct correlation to the target being tracked. Depending on the target being tracked, the direct correlation relationship between the target and the marker will vary. For example, in long bones, the marker may be place anywhere along the bone to provide motion that directly correlations to target motion in the bone. With respect to soft tissue that moves substantially in response to the bony anatomy, for example, the head and neck, the marker may be placed in a bite block to provide surrogate motion in direct correlation with target motion. With respect to soft tissue and as discussed in detail above, the target may be placed in adjacent soft tissue to provide a surrogate having direct correlation to target motion.
FIG. 4 is a flow diagram illustrating several aspects and uses of real time tracking to monitor the location and the status of the target. In this embodiment, anintegrated method90 for radiation therapy includes aradiation planning procedure91 that determines the plan for applying the radiation to the patient over a number of radiation fractions. Theradiation planning procedure91 typically includes an imaging stage in which images of a tumor or other types of targets are obtained using X-rays, CT, MRI, or ultrasound imaging. The images are analyzed by a person to measure the relative distances between the markers and the relative position between the target and the markers.FIG. 5A, for example, is a representation of a CT image showing a cross-section of thepatient6, thetarget2, and amarker40. Referring toFIG. 5B, the coordinates (x0, y0, z0) of themarker40 in a reference frame RCTof the CT scanner can be determined by an operator. The coordinates of the tumor can be determined in a similar manner to ascertain the offset between the marker and the target.
Theradiation planning procedure91 can also include tracking the targets using the localization system10 (FIG. 3) in an observation area separate from the imaging equipment. The markers40 (FIG. 3) can be tracked to identify changes in the configuration (e.g., size/shape) of the target over time and to determine the trajectory of the target caused by movement of the target within the patient (e.g., simulation). For many treatment plans, the computer does not need to provide objective output data of the marker or target locations to a user in real time, but rather the data can be recorded in real time. Based on the images obtained during the imaging stage and the additional data obtained by tracking the markers using thelocalization system10 in a simulation procedure, a treatment plan is developed for applying the radiation to the target.
Thelocalization system10 and themarkers40 enable an automated patient setup process for delivering the radiation. After developing a treatment plan, themethod90 includes asetup procedure92 in which the patient is positioned on a movable support table so that the target and markers are generally adjacent to the sensor assembly. As described above, the excitation source is activated to energize the markers, and the sensors measure the strength of the signals from the markers. The computer controller then (a) calculates objective values of the locations of the markers and the target relative to the machine isocenter, and (b) determines an objective offset value between the position of the target and the machine isocenter. Referring toFIG. 6, for example, the objective offset values can be provided to a user interface that displays the vertical, lateral and longitudinal offsets of the target relative to the machine isocenter. A user interface may, additionally or instead, display target rotation.
One aspect of several embodiments of thelocalization system10 is that the objective values are provided to the user interface or other device by processing the position data from thefield sensor70 in thecontroller80 or other computer without human interpretation of the data received by thefield sensor70. If the offset value is outside of an acceptable range, the computer automatically activates the control system of the support table to move the tabletop relative to the machine isocenter until the target isocenter is coincident with the machine isocenter. The computer controller generally provides the objective output data of the offset to the table control system in real time as defined above. For example, because the output is provided to the radiation delivery device, it can be at a high rate (1-20 ms) and a low latency (10-20 ms). If the output data is provided to a user interface in addition to or in lieu of the table controller, it can be at a relatively lower rate (20-50 ms) and higher latency (50-200 ms).
In one embodiment, the computer controller also determines the position and orientation of the markers relative to the position and orientation of simulated markers. The locations of the simulated markers are selected so that the target will be at the machine isocenter when the real markers are at the selected locations for the simulated markers. If the markers are not properly aligned and oriented with the simulated markers, the support table is adjusted as needed for proper marker alignment. This marker alignment properly positions the target along six dimensions, namely X, Y, Z, pitch, yaw, and roll. Accordingly, the patient is automatically positioned in the correct position and rotation relative to the machine isocenter for precise delivery of radiation therapy to the target.
Referring back toFIG. 4, themethod90 further includes aradiation session93.FIG. 7 shows a further aspect of an automated process in which thelocalization system10 tracks the target during theradiation session93 and controls theradiation delivery device20 according to the offset between target and the machine isocenter. For example, if the position of the target is outside of a permitted degree or range of displacement from the machine isocenter, thelocalization system10 sends a signal to interrupt the delivery of the radiation or prevent initial activation of the beam. In another embodiment, thelocalization system10 sends signals to automatically reposition atabletop27 and the patient6 (as a unit) so that the target isocenter remains within a desired range of the machine isocenter during theradiation session93 even if the target moves. In still another embodiment, thelocalization system10 sends signals to activate the radiation only when the target is within a desired range of the machine isocenter (e.g., gated therapy). In the case of treating a target in the lung, one embodiment of gated therapy includes tracking the target during inspiration/expiration, having the patient hold his/her breath at the end of an inspiration/expiration cycle, and activating thebeam21 when thecomputer80 determines that the objective offset value between the target and the machine isocenter is within a desired range. Accordingly, the localization system enables dynamic adjustment of the table27 and/or thebeam21 in real time while irradiating the patient. This is expected to ensure that the radiation is accurately delivered to the target without requiring a large margin around the target.
The localization system provides the objective data of the offset and/or rotation to the linear accelerator and/or the patient support table in real time as defined above. For example, as explained above with respect to automatically positioning the patent support table during thesetup procedure92, the localization system generally provides the objective output to the radiation delivery device at least substantially contemporaneously with obtaining the position data of the markers and/or at a sufficient frequency to track the target in real time. The objective output, for example, can be provided at a short periodicity (1-20 ms) and a low latency (10-20 ms) such that signals for controlling thebeam21 can be sent to theradiation delivery device20 in the same time periods during a radiation session. In another example of real time tracking, the objective output is provided a plurality of times during an “on-beam” period (e.g., 2, 5, 10 or more times while the beam is on). In the case of terminating or activating the radiation beam, or adjusting the leafs of a beam collimator, it is generally desirable to maximize the refresh rate and minimize the latency. In some embodiments, therefore, the localization system may provide the objective output data of the target location and/or the marker locations at a periodicity of 10 ms or less and a latency of 10 ms or less.
Themethod90 further includes averification procedure94 in which the real time objective output data from theradiation session93 is compared to the status of the parameters of the radiation beam. For example, the target locations can be correlated with the beam intensity, beam position, and collimator configuration at corresponding time intervals during theradiation session93. This correlation can be used to determine the dose of radiation delivered to discrete regions in and around the target. This information can also be used to determine the effects of radiation on certain areas of the target by noting changes in the target configuration or the target trajectory.
Themethod90 can further include a first decision (Block95) in which the data from theverification procedure94 is analyzed to determine whether the treatment is complete. If the treatment is not complete, themethod90 further includes a second decision (Block96) in which the results of the verification procedure are analyzed to determine whether the treatment plan should be revised to compensate for changes in the target. If revisions are necessary, the method can proceed with repeating theplanning procedure91. On the other hand, if the treatment plan is providing adequate results, themethod90 can proceed by repeating thesetup procedure92,radiation session93, andverification procedure94 in a subsequent fraction of the radiation therapy.
Thelocalization system10 provides several features, either individually or in combination with each other, that enhance the ability to accurately deliver high doses of radiation to targets within tight margins. For example, many embodiments of the localization system use leadless markers that are implanted in the patient so that they are substantially fixed with respect to the target. The markers accordingly move either directly with the target or in a relationship proportional to the movement of the target. As a result, internal movement of the target caused by respiration, organ filling, cardiac functions, or other factors can be identified and accurately tracked before, during and after medical procedures. Moreover, many aspects of thelocalization system10 use a non-ionizing energy to track the leadless markers in an external, absolute reference frame in a manner that provides objective output. In general, the objective output is determined in a computer system without having a human interpret data (e.g., images) while thelocalization system10 tracks the target and provides the objective output. This significantly reduces the latency between the time when the position of the marker is sensed and the objective output is provided to a device or a user. For example, this enables an objective output responsive to the location of the target to be provided at least substantially contemporaneously with collecting the position data of the marker. The system also effectively eliminates inter-user variability associated with subjective interpretation of data (e.g., images).
D. Specific Embodiments of Markers and Localization Systems
The following specific embodiments of markers, excitation sources, sensors and controllers provide additional details to implement the systems and processes described above with reference toFIGS. 1-7. The present inventors overcame many challenges to develop markers and localization systems that accurately determine the location of a marker which (a) produces a wirelessly transmitted location signal in response to a wirelessly transmitted excitation energy, and (b) has a cross-section small enough to be implanted in the lung, prostate, or other part of a patient. Systems with these characteristics have several practical advantages, including (a) not requiring ionization radiation, (b) not requiring line-of-sight between the markers and sensors, and (c) effecting an objective measurement of a target's location and/or rotation. The following specific embodiments are described in sufficient detail to enable a person skilled in the art to make and use such a localization system for radiation therapy involving a tumor in the patient, but the invention is not limited to the following embodiments of markers, excitation sources, sensor assemblies and/or controllers.
1. Markers
FIG. 8A is an isometric view of amarker100 for use with the localization system10 (FIGS. 1-7). The embodiment of themarker100 shown inFIG. 8A includes acasing110 and a magnetic transponder120 (e.g., a resonating circuit) in thecasing110. Thecasing110 is a barrier configured to be implanted in the patient, or encased within the body of an instrument. Thecasing110 can alternatively be configured to be adhered externally to the skin of the patient. Thecasing110 can be a generally cylindrical capsule that is sized to fit within the bore of a small introducer, such as bronchoscope or percutaneous trans-thoracic implanter, but thecasing110 can have other configurations and be larger or smaller. Thecasing110, for example, can have barbs or other features to anchor thecasing110 in soft tissue or an adhesive for attaching thecasing110 externally to the skin of a patient. Suitable anchoring mechanisms for securing themarker100 to a patient are disclosed in International Publication No. WO 02/39917 A1, which designates the United States and is incorporated herein by reference. In one embodiment, thecasing110 includes (a) a capsule or shell112 having aclosed end114 and anopen end116, and (b) asealant118 in theopen end116 of theshell112. Thecasing110 and thesealant118 can be made from plastics, ceramics, glass or other suitable biocompatible materials.
Themagnetic transponder120 can include a resonating circuit that wirelessly transmits a location signal in response to a wirelessly transmitted excitation field as described above. In this embodiment, themagnetic transponder120 comprises acoil122 defined by a plurality of windings of aconductor124. Many embodiments of themagnetic transponder120 also include acapacitor126 coupled to thecoil122. Thecoil122 resonates at a selected resonant frequency. Thecoil122 can resonate at a resonant frequency solely using the parasitic capacitance of the windings without having a capacitor, or the resonant frequency can be produced using the combination of thecoil122 and thecapacitor126. Thecoil122 accordingly generates an alternating magnetic field at the selected resonant frequency in response to the excitation energy either by itself or in combination with thecapacitor126. Theconductor124 of the illustrated embodiment can be hot air or alcohol bonded wire having a gauge of approximately 45-52. Thecoil122 can have 800-1000 turns, and the windings are preferably wound in a tightly layered coil. Themagnetic transponder120 can further include acore128 composed of a material having a suitable magnetic permeability. For example, thecore128 can be a ferromagnetic element composed of ferrite or another material. Themagnetic transponder120 can be secured to thecasing110 by an adhesive129.
Themarker100 also includes an imaging element that enhances the radiographic image of the marker to make the marker more discernible in radiographic images. The imaging element also has a radiographic profile in a radiographic image such that the marker has a radiographic centroid at least approximately coincident with the magnetic centroid of themagnetic transponder120. As explained in more detail below, the radiographic and magnetic centroids do not need to be exactly coincident with each other, but rather can be within an acceptable range.
FIG. 8B is a cross-sectional view of themarker100 along line8B-8B ofFIG. 8A that illustrates animaging element130 in accordance with an embodiment of the invention. Theimaging element130 illustrated in FIGS.8A-B includes afirst contrast element132 andsecond contrast element134. The first andsecond contrast elements132 and134 are generally configured with respect to themagnetic transponder120 so that themarker100 has a radiographic centroid Rcthat is at least substantially coincident with the magnetic centroid Mcof themagnetic transponder120. For example, when theimaging element130 includes two contrast elements, the contrast elements can be arranged symmetrically with respect to themagnetic transponder120 and/or each other. The contrast elements can also be radiographically distinct from themagnetic transponder120. In such an embodiment, the symmetrical arrangement of distinct contrast elements enhances the ability to accurately determine the radiographic centroid of themarker100 in a radiographic image.
The first andsecond contrast elements132 and134 illustrated in FIGS.8A-B are continuous rings positioned at opposing ends of thecore128. Thefirst contrast element132 can be at or around afirst end136aof thecore128, and thesecond contrast element134 can be at or around asecond end136bof thecore128. The continuous rings shown in FIGS.8A-B have substantially the same diameter and thickness. The first andsecond contrast elements132 and134, however, can have other configurations and/or be in other locations relative to thecore128 in other embodiments. For example, the first andsecond contrast elements132 and134 can be rings with different diameters and/or thicknesses.
The radiographic centroid of the image produced by theimaging element130 does not need to be absolutely coincident with the magnetic centroid Mc, but rather the radiographic centroid and the magnetic centroid should be within an acceptable range. For example, the radiographic centroid Rccan be considered to be at least approximately coincident with the magnetic centroid Mcwhen the offset between the centroids is less than approximately 5 mm. In more stringent applications, the magnetic centroid Mcand the radiographic centroid Rcare considered to be at least substantially coincident with each other when the offset between the centroids is 2 mm, or less than 1 mm. In other applications, the magnetic centroid Mcis at least approximately coincident with the radiographic centroid Rcwhen the centroids are spaced apart by a distance not greater than half the length of themagnetic transponder120 and/or themarker100.
Theimaging element130 can be made from a material and configured appropriately to absorb a high fraction of incident photons of a radiation beam used for producing the radiographic image. For example, when the imaging radiation has high acceleration voltages in the megavoltage range, theimaging element130 is made from, at least in part, high density materials with sufficient thickness and cross-sectional area to absorb enough of the photon fluence incident on the imaging element to be visible in the resulting radiograph. Many high energy beams used for therapy have acceleration voltages of 6 MV-25 MV, and these beams are often used to produce radiographic images in the 5 MV-10 MV range, or more specifically in the 6 MV-8 MV range. As such, theimaging element130 can be made from a material that is sufficiently absorbent of incident photon fluence to be visible in an image produced using a beam with an acceleration voltage of 5 MV-10 MV, or more specifically an acceleration voltage of 6 MV-8 MV.
Several specific embodiments ofimaging elements130 can be made from gold, tungsten, platinum and/or other high density metals. In these embodiments theimaging element130 can be composed of materials having a density of 19.25 g/cm3 (density of tungsten) and/or a density of approximately 21.4 g/cm3 (density of platinum). Many embodiments of theimaging element130 accordingly have a density not less than 19 g/cm3. In other embodiments, however, the material(s) of theimaging element130 can have a substantially lower density. For example, imaging elements with lower density materials are suitable for applications that use lower energy radiation to produce radiographic images. Moreover, the first andsecond contrast elements132 and134 can be composed of different materials such that thefirst contrast element132 can be made from a first material and thesecond contrast element134 can be made from a second material.
Referring toFIG. 8B, themarker100 can further include amodule140 at an opposite end of the core128 from thecapacitor126. In the embodiment of themarker100 shown inFIG. 8B, themodule140 is configured to be symmetrical with respect to thecapacitor126 to enhance the symmetry of the radiographic image. As with the first andsecond contrast elements132 and134, themodule140 and thecapacitor126 are arranged such that the magnetic centroid of the marker is at least approximately coincident with the radiographic centroid of themarker100. Themodule140 can be another capacitor that is identical to thecapacitor126, or themodule140 can be an electrically inactive element. Suitable electrically inactive modules include ceramic blocks shaped like thecapacitor126 and located with respect to thecoil122, thecore128 and theimaging element130 to be symmetrical with each other. In still other embodiments themodule140 can be a different type of electrically active element electrically coupled to themagnetic transponder120.
One specific process of using the marker involves imaging the marker using a first modality and then tracking the target of the patient and/or the marker using a second modality. For example, the location of the marker relative to the target can be determined by imaging the marker and the target using radiation. The marker and/or the target can then be localized and tracked using the magnetic field generated by the marker in response to an excitation energy.
Themarker100 shown in FIGS.8A-B is expected to provide an enhanced radiographic image compared to conventional magnetic markers for more accurately determining the relative position between the marker and the target of a patient.FIG. 8C, for example, illustrates aradiographic image150 of themarker100 and a target T of the patient. The first andsecond contrast elements132 and134 are expected to be more distinct in theradiographic image150 because they can be composed of higher density materials than the components of themagnetic transponder120. The first andsecond contrast elements132 and134 can accordingly appear as bulbous ends of a dumbbell shape in applications in which the components of themagnetic transponder120 are visible in the image. In certain megavolt applications, the components of themagnetic transponder120 may not appear at all on theradiographic image150 such that the first andsecond contrast elements132 and134 will appear as distinct regions that are separate from each other. In either embodiment, the first andsecond contrast elements132 and134 provide a reference frame in which the radiographic centroid Rcof themarker100 can be located in theimage150. Moreover, because theimaging element130 is configured so that the radiographic centroid Rcis at least approximately coincident with the magnetic centroid Mc, the relative offset or position between the target T and the magnetic centroid Mccan be accurately determined using themarker100. The embodiment of themarker100 illustrated in FIGS.8A-C, therefore, is expected to mitigate errors caused by incorrectly estimating the radiographic and magnetic centroids of markers in radiographic images.
FIG. 9A is an isometric view of amarker200 with a cut-away portion to illustrate internal components, andFIG. 9B is a cross-sectional view of themarker200 taken alongline9B-9B ofFIG. 9A. Themarker200 is similar to themarker100 shown above inFIG. 8A, and thus like reference numbers refer to like components. Themarker200 differs from themarker100 in that themarker200 includes animaging element230 defined by a single contrast element. Theimaging element230 is generally configured relative to themagnetic transponder120 so that the radiographic centroid of themarker200 is at least approximately coincident with the magnetic centroid of themagnetic transponder120. Theimaging element230, more specifically, is a ring extending around thecoil122 at a medial region of themagnetic transponder120. Theimaging element230 can be composed of the same materials described above with respect to theimaging element130 in FIGS.8A-B. Theimaging element230 can have an inner diameter that is approximately equal to the outer diameter of thecoil122, and an outer diameter within thecasing110. As shown inFIG. 9B, however, aspacer231 can be between the inner diameter of theimaging element230 and the outer diameter of thecoil122.
Themarker200 is expected to operate in a manner similar to themarker100 described above. Themarker200, however, does not have two separate contrast elements that provide two distinct, separate points in a radiographic image. Theimaging element230 is still highly useful in that it identifies the radiographic centroid of themarker200 in a radiographic image, and it can be configured so that the radiographic centroid of themarker200 is at least approximately coincident with the magnetic centroid of themagnetic transponder120.
FIG. 10A is an isometric view of amarker300 having a cut-away portion, andFIG. 10B is a cross-sectional view of themarker300 taken alongline10B-10B ofFIG. 10A. Themarker300 is substantially similar to themarker200 shown in FIGS.9A-B, and thus like reference numbers refer to like components inFIGS. 8A-10B. Theimaging element330 can be a high density ring configured relative to themagnetic transponder120 so that the radiographic centroid of themarker300 is at least approximately coincident with the magnetic centroid of themagnetic transponder120. Themarker300, more specifically, includes animaging element330 around thecasing110. Themarker300 is expected to operate in much the same manner as themarker200 shown in FIGS.9A-B.
FIG. 11 is an isometric view with a cut-away portion illustrating amarker400 in accordance with another embodiment of the invention. Themarker400 is similar to themarker100 shown in FIGS.8A-C, and thus like reference numbers refer to like components in these Figures. Themarker400 has animaging element430 including afirst contrast element432 at one end of themagnetic transponder120 and asecond contrast element434 at another end of themagnetic transponder120. The first andsecond contrast elements432 and434 are spheres composed of suitable high density materials. Thecontrast elements432 and434, for example, can be composed of gold, tungsten, platinum or other suitable high-density materials for use in radiographic imaging. Themarker400 is expected to operate in a manner similar to themarker100, as described above.
FIG. 12 is an isometric view with a cut-away portion of amarker500 in accordance with yet another embodiment of the invention. Themarker500 is substantially similar to themarkers100 and400 shown inFIGS. 8A and 11, and thus like reference numbers refer to like components in these Figures. Themarker500 includes animaging element530 including afirst contrast element532 and asecond contrast element534. The first andsecond contrast elements532 and534 can be positioned proximate to opposing ends of themagnetic transponder120. The first andsecond contrast elements532 and534 can be discontinuous rings having agap535 to mitigate eddy currents. Thecontrast elements532 and534 can be composed of the same materials as described above with respect to the contrast elements of other imaging elements in accordance with other embodiments of the invention.
Additional embodiments of markers in accordance with the invention can include imaging elements incorporated into or otherwise integrated with thecasing110, the core128 (FIG. 8B) of themagnetic transponder120, and/or the adhesive129 (FIG. 8B) in the casing. For example, particles of a high density material can be mixed with ferrite and extruded to form thecore128. Alternative embodiments can mix particles of a high density material with glass or another material to form thecasing110, or coat thecasing110 with a high-density material. In still other embodiments, a high density material can be mixed with the adhesive129 and injected into thecasing110. Any of these embodiments can incorporate the high density material into a combination of thecasing110, thecore128 and/or the adhesive129. Suitable high density materials can include tungsten, gold and/or platinum as described above.
The markers described above with reference toFIGS. 8A-12 can be used for themarkers40 in the localization system10 (FIGS. 1-7). Thelocalization system10 can have several markers with the same type of imaging elements, or markers with different imaging elements can be used with the same instrument. Several additional details of these markers and other embodiments of markers are described in U.S. application Ser. Nos. 10/334,698 and 10/746,888, which are incorporated herein by reference. For example, the markers may not have any imaging elements for applications with lower energy radiation, or the markers may have reduced volumes of ferrite and metals to mitigate issues with MRI imaging as set forth in U.S. application Ser. No. 10/334,698.
2. Localization Systems
FIG. 13 is a schematic block diagram of alocalization system1000 for determining the absolute location of the markers40 (shown schematically) relative to a reference frame. Thelocalization system1000 includes anexcitation source1010, asensor assembly1012, asignal processor1014 operatively coupled to thesensor assembly1012, and acontroller1016 operatively coupled to theexcitation source1010 and thesignal processor1014. Theexcitation source1010 is one embodiment of theexcitation source60 described above with reference toFIG. 3; thesensor assembly1012 is one embodiment of thesensor assembly70 described above with reference toFIG. 3; and thecontroller1016 is one embodiment of thecontroller80 described above with reference toFIG. 3.
Theexcitation source1010 is adjustable to generate a magnetic field having a waveform with energy at selected frequencies to match the resonant frequencies of themarkers40. The magnetic field generated by theexcitation source1010 energizes the markers at their respective frequencies. After themarkers40 have been energized, theexcitation source1010 is momentarily switched to an “off” position so that the pulsed magnetic excitation field is terminated while the markers wirelessly transmit the location signals. This allows thesensor assembly1012 to sense the location signals from themarkers40 without measurable interference from the significantly more powerful magnetic field from theexcitation source1010. Theexcitation source1010 accordingly allows thesensor assembly1012 to measure the location signals from themarkers40 at a sufficient signal-to-noise ratio so that thesignal processor1014 or thecontroller1016 can accurately calculate the absolute location of themarkers40 relative to a reference frame.
a. Excitation Sources
Referring still toFIG. 13, theexcitation source1010 includes a highvoltage power supply1040, anenergy storage device1042 coupled to thepower supply1040, and aswitching network1044 coupled to theenergy storage device1042. Theexcitation source1010 also includes acoil assembly1046 coupled to theswitching network1044. In one embodiment, thepower supply1040 is a 500 volt power supply, although other power supplies with higher or lower voltages can be used. Theenergy storage device1042 in one embodiment is a high voltage capacitor that can be charged and maintained at a relatively constant charge by thepower supply1040. Theenergy storage device1042 alternately provides energy to and receives energy from the coils in thecoil assembly1046.
Theenergy storage device1042 is capable of storing adequate energy to reduce voltage drop in the energy storage device while having a low series resistance to reduce power losses. Theenergy storage device1042 also has a low series inductance to more effectively drive thecoil assembly1046. Suitable capacitors for theenergy storage device1042 include aluminum electrolytic capacitors used in flash energy applications. Alternative energy storage devices can also include NiCd and lead acid batteries, as well as alternative capacitor types, such as tantalum, film, or the like.
Theswitching network1044 includes individual H-bridge switches1050 (identified individually by reference numbers1050a-d), and thecoil assembly1046 includes individual source coils1052 (identified individually by reference numbers1052a-d). Each H-bridge switch1050 controls the energy flow between theenergy storage device1042 and one of the source coils1052. For example, H-bridge switch #11050aindependently controls the flow of the energy to/fromsource coil #11052a, H-bridge switch #21050bindependently controls the flow of the energy to/fromsource coil #21052b, H-bridge switch #31050cindependently controls the flow of the energy to/fromsource coil #31052c, and H-bridge switch #41050dindependently controls the flow of the energy to/fromsource coil #41052d. Theswitching network1044 accordingly controls the phase of the magnetic field generated by each of the source coils1052a-dindependently. The H-bridges1050 can be configured so that the electrical signals for all the source coils1052 are in phase, or the H-bridge switches1050 can be configured so that one or more of the source coils1052 are 180° out of phase. Furthermore, the H-bridge switches1050 can be configured so that the electrical signals for one or more of the source coils1052 are between 0 and 180° out of phase to simultaneously provide magnetic fields with different phases.
The source coils1052 can be arranged in a coplanar array that is fixed relative to the reference frame. Each source coil1052 can be a square, planar winding arranged to form a flat, substantially rectilinear coil. The source coils1052 can have other shapes and other configurations in different embodiments. In one embodiment, the source coils1052 are individual conductive lines formed in a stratum of a printed circuit board, or windings of a wire in a foam frame. Alternatively, the source coils1052 can be formed in different substrates or arranged so that two or more of the source coils are not planar with each other. Additionally, alternate embodiments of the invention may have fewer or more source coils than illustrated inFIG. 13.
The selected magnetic fields from the source coils1052 combine to form an adjustable excitation field that can have different three-dimensional shapes to excite themarkers40 at any spatial orientation within an excitation volume. When the planar array of the source coils1052 is generally horizontal, the excitation volume is positioned above an area approximately corresponding to the central region of thecoil assembly1046. The excitation volume is the three-dimensional space adjacent to thecoil assembly1046 in which the strength of the magnetic field is sufficient to adequately energize themarkers40.
FIGS. 14-16 are schematic views of a planar array of the source coils1052 with the alternating electrical signals provided to the source coils in different combinations of phases to generate excitation fields about different axes relative to the illustrated XYZ coordinate system. Each source coil1052 has twoouter sides1112 and twoinner sides1114. Eachinner side1114 of one source coil1052 is immediately adjacent to aninner side1114 of another source coil1052, but theouter sides1112 of all the source coils1052 are not adjacent to any other source coil1052.
In the embodiment ofFIG. 14, all the source coils1052a-dsimultaneously receive an alternating electrical signals in the same phase. As a result, the electrical current flows in the same direction through all the source coils1052a-dsuch that adirection1113 of the current flowing along theinner sides1114 of one source coil (e.g.,source coil1052a) is opposite to thedirection1113 of the current flowing along theinner sides1114 of the two adjacent source coils (e.g., source coils1052cand1052d). The magnetic fields generated along theinner sides1114 accordingly cancel each other out so that the magnetic field is effectively generated from the current flowing along theouter sides1112 of the source coils. The resulting excitation field formed by the combination of the magnetic fields from the source coils1052a-dshown inFIG. 14 has amagnetic moment1115 generally in the Z direction within anexcitation volume1109. This excitation field energizes markers parallel to the Z-axis or markers positioned with an angular component along the Z-axis (i.e., not orthogonal to the Z-axis).
FIG. 15 is a schematic view of the source coils1052a-dwith the alternating electrical signals provided in a second combination of phases to generate a second excitation field with a different spatial orientation. In this embodiment, source coils1052aand1052care in phase with each other, andsource coils1052band1052dare in phase with each other. However, source coils1052aand1052care 180 degrees out of phase withsource coils1052band1052d. The magnetic fields from the source coils1052a-dcombine to generate an excitation field having amagnetic moment1217 generally in the Y direction within theexcitation volume1109. Accordingly, this excitation field energizes markers parallel to the Y-axis or markers positioned with an angular component along the Y-axis.
FIG. 16 is a schematic view of the source coils1052a-dwith the alternating electrical signals provided in a third combination of phases to generate a third excitation field with a different spatial orientation. In this embodiment, source coils1052aand1052bare in phase with each other, andsource coils1052cand1052dare in phase with each other. However, source coils1052aand1052bare 180 degrees out of phase withsource coils1052cand1052d. The magnetic fields from the source coils1052a-dcombine to generate an excitation field having amagnetic moment1319 in theexcitation volume1109 generally in the direction of the X-axis. Accordingly, this excitation field energizes markers parallel to the X-axis or markers positioned with an angular component along the X-axis.
FIG. 17 is a schematic view of the source coils1052a-dillustrating the current flow to generate anexcitation field1424 for energizingmarkers40 with longitudinal axes parallel to the Y-axis. The switching network1044 (FIG. 13) is configured so that the phases of the alternating electrical signals provided to the source coils1052a-dare similar to the configuration ofFIG. 15. This generates theexcitation field1424 with a magnetic moment in the Y direction to energize themarkers40.
FIG. 18 further illustrates the ability to spatially adjust the excitation field in a manner that energizes any of themarkers40 at different spatial orientations. In this embodiment, the switching network1044 (FIG. 13) is configured so that the phases of the alternating electrical signals provided to the source coils1052a-dare similar to the configuration shown inFIG. 14. This produces an excitation field with a magnetic moment in the Z direction that energizesmarkers40 with longitudinal axes parallel to the Z-axis.
The spatial configuration of the excitation field in theexcitation volume1109 can be quickly adjusted by manipulating the switching network to change the phases of the electrical signals provided to the source coils1052a-d. As a result, the overall magnetic excitation field can be changed to be oriented in either the X, Y or Z directions within theexcitation volume1109. This adjustment of the spatial orientation of the excitation field reduces or eliminates blind spots in theexcitation volume1109. Therefore, themarkers40 within theexcitation volume1109 can be energized by the source coils1052a-dregardless of the spatial orientations of the leadless markers.
In one embodiment, theexcitation source1010 is coupled to thesensor assembly1012 so that the switching network1044 (FIG. 13) adjusts orientation of the pulsed generation of the excitation field along the X, Y, and Z axes depending upon the strength of the signal received by the sensor assembly. If the location signal from amarker40 is insufficient, theswitching network1044 can automatically change the spatial orientation of the excitation field during a subsequent pulsing of the source coils1052a-dto generate an excitation field with a moment in the direction of a different axis or between axes. Theswitching network1044 can be manipulated until thesensor assembly1012 receives a sufficient location signal from the marker.
Theexcitation source1010 illustrated inFIG. 13 alternately energizes the source coils1052a-dduring an excitation phase to power themarkers40, and then actively de-energizes the source coils1052a-dduring a sensing phase in which thesensor assembly1012 senses the decaying location signals wirelessly transmitted by themarkers40. To actively energize and de-energize the source coils1052a-d, theswitching network1044 is configured to alternatively transfer stored energy from theenergy storage device1042 to the source coils1052a-d, and to then re-transfer energy from the source coils1052a-dback to theenergy storage device1042. Theswitching network1044 alternates between first and second “on” positions so that the voltage across the source coils1052 alternates between positive and negative polarities. For example, when theswitching network1044 is switched to the first “on” position, the energy in theenergy storage device1042 flows to the source coils1052a-d. When theswitching network1044 is switched to the second “on” position, the polarity is reversed such that the energy in the source coils1052a-dis actively drawn from the source coils1052a-dand directed back to theenergy storage device1042. As a result, the energy in the source coils1052a-dis quickly transferred back to theenergy storage device1042 to abruptly terminate the excitation field transmitted from the source coils1052a-dand to conserve power consumed by theenergy storage device1042. This removes the excitation energy from the environment so that thesensor assembly1012 can sense the location signals from themarkers40 without interference from the significantly larger excitation energy from theexcitation source1010. Several additional details of theexcitation source1010 and alternate embodiments are disclosed in U.S. patent application Ser. No. 10/213,980 filed on Aug. 7, 2002, and now U.S. Pat. No. 6,822,570, which is incorporated by reference herein in its entirety.
b. Sensor Assemblies
FIG. 19A is an exploded isometric view showing several components of thesensor assembly1012 for use in the localization system1000 (FIG. 13). Thesensor assembly1012 includes asensing unit1601 having a plurality ofcoils1602 formed on or carried by apanel1604. Thecoils1602 can be field sensors or magnetic flux sensors arranged in asensor array1605.
Thepanel1604 may be a substantially non-conductive material, such as a sheet of KAPTON® produced by DuPont. KAPTON® is particularly useful when an extremely stable, tough, and thin film is required (such as to avoid radiation beam contamination), but thepanel1604 may be made from other materials and have other configurations. For example, FR4 (epoxy-glass substrates), GETEK or other Teflon-based substrates, and other commercially available materials can be used for thepanel1604. Additionally, although thepanel1604 may be a flat, highly planar structure, in other embodiments, the panel may be curved along at least one axis. In either embodiment, the field sensors (e.g., coils) are arranged in a locally planar array in which the plane of one field sensor is at least substantially coplanar with the planes of adjacent field sensors. For example, the angle between the plane defined by one coil relative to the planes defined by adjacent coils can be from approximately 0° to 10°, and more generally is less than 5°. In some circumstances, however, one or more of the coils may be at an angle greater than 10° relative to other coils in the array.
Thesensor assembly1012 shown inFIG. 19A can optionally include acore1620 laminated to thepanel1604. Thecore1620 can be a support member made from a rigid material, or thecore1620 can be a low density foam, such as a closed-cell Rohacell foam. Thecore1620 is preferably a stable layer that has a low coefficient of thermal expansion so that the shape of thesensor assembly1012 and the relative orientation between thecoils1602 remain within a defined range over an operating temperature range.
Thesensor assembly1012 can further include afirst exterior cover1630aon one side of the sensing subsystem and asecond exterior cover1630bon an opposing side. The first and second exterior covers1630a-bcan be thin, thermally stable layers, such as Kevlar or Thermount films. Each of the first and second exterior covers1630a-bcan includeelectric shielding1632 to block undesirable external electric fields from reaching thecoils1602. Theelectric shielding1632 can be a plurality of parallel legs of gold-plated, copper strips to define a comb-shaped shield in a configuration commonly called a Faraday shield. It will be appreciated that the shielding can be formed from other materials that are suitable for shielding. The electric shielding can be formed on the first and second exterior covers using printed circuit board manufacturing technology or other techniques.
Thepanel1604 with thecoils1602 is laminated to thecore1620 using a pressure sensitive adhesive or another type of adhesive. The first and second exterior covers1630a-bare similarly laminated to the assembly of thepanel1604 and thecore1620. The laminated assembly forms a rigid structure that fixedly retains the arrangement of thecoils1602 in a defined configuration over a large operating temperature range. As such, thesensor assembly1012 does not substantially deflect across its surface during operation. Thesensor assembly1012, for example, can retain the array ofcoils1602 in the fixed position with a deflection of no greater than ±0.5 mm, and in some cases no more than ±0.3 mm. The stiffness of the sensing subsystem provides very accurate and repeatable monitoring of the precise location of leadless markers in real time.
In still another embodiment, thesensor assembly1012 can further include a plurality of source coils that are a component of theexcitation source1010. One suitable array combining thesensor assembly1012 with source coils is disclosed in U.S. patent application Ser. No. 10/334,700, entitled PANEL-TYPE SENSOR/SOURCE ARRAY ASSEMBLY, filed on Dec. 30, 2002, which is herein incorporated by reference.
FIG. 19B further illustrates an embodiment of thesensing unit1601. In this embodiment, thesensing unit1601 includes 32sensor coils1602; eachcoil1602 is associated with a separate channel1606 (shown individually as channels “Ch 0” through “Ch 31”). The overall dimension of thepanel1604 can be approximately 40 cm by 54 cm, but thearray1605 has a first dimension D1 of approximately 40 cm and a second dimension D2 of approximately 40 cm. Thearray1605 can have other sizes or other configurations (e.g., circular) in alternative embodiments. Additionally, thearray1605 can have more or fewer coils, such as 8-64 coils; the number of coils may moreover be a power of 2.
Thecoils1602 may be conductive traces or depositions of copper or another suitably conductive metal formed on thepanel1604. Eachcoil1602 has a trace with a width of approximately 0.15 mm and a spacing between adjacent turns within each coil of approximately 0.13 mm. Thecoils1602 can have approximately 15 to 90 turns, and in specific applications each coil has approximately 40 turns. Coils with less than 15 turns may not be sensitive enough for some applications, and coils with more than 90 turns may lead to excessive voltage from the source signal during excitation and excessive settling times resulting from the coil's lower self-resonant frequency. In other applications, however, thecoils1602 can have less than 15 turns or more than 90 turns.
As shown inFIG. 19B, thecoils1602 are arranged as square spirals, although other configurations may be employed, such as arrays of circles, interlocking hexagons, triangles, etc. Such square spirals utilize a large percentage of the surface area to improve the signal to noise ratio. Square coils also simplify design layout and modeling of the array compared to circular coils; for example, circular coils could waste surface area for linking magnetic flux from themarkers40. Thecoils1602 have an inner dimension of approximately 40 mm, and an outer dimension of approximately 62 mm, although other dimensions are possible depending upon applications. Sensitivity may be improved with an inner dimension as close to an outer dimension as possible given manufacturing tolerances. In several embodiments, thecoils1602 are identical to each other or at least configured substantially similarly.
The pitch of thecoils1602 in thearray1605 is a function of, at least in part, the minimum distance between the marker and the coil array. In one embodiment, the coils are arranged at a pitch of approximately 67 mm. This specific arrangement is particularly suitable when thewireless markers40 are positioned approximately 7-27 cm from thesensor assembly1012. If the wireless markers are closer than 7 cm, then the sensing subsystem may include sensor coils arranged at a smaller pitch. In general, a smaller pitch is desirable when wireless markers are to be sensed at a relatively short distance from the array of coils. The pitch of thecoils1602, for example, is approximately 50%-200% of the minimum distance between the marker and the array.
In general, the size and configuration of thearray1605 and thecoils1602 in the array depend on the frequency range in which they are to operate, the distance from themarkers40 to the array, the signal strength of the markers, and several other factors. Those skilled in the relevant art will readily recognize that other dimensions and configurations may be employed depending, at least in part, on a desired frequency range and distance from the markers to the coils.
Thearray1605 is sized to provide a large aperture to measure the magnetic field emitted by the markers. It can be particularly challenging to accurately measure the signal emitted by an implantable marker that wirelessly transmits a marker signal in response to a wirelessly transmitted energy source because the marker signal is much smaller than the source signal and other magnetic fields in a room (e.g., magnetic fields from CRTs, etc.). The size of thearray1605 can be selected to preferentially measure the near field of the marker while mitigating interference from far field sources. In one embodiment, thearray1605 is sized to have a maximum dimension D1 or D2 across the surface of the area occupied by the coils that is approximately 100% to 300% of a predetermined maximum sensing distance that the markers are to be spaced from the plane of the coils. Thus, the size of thearray1605 is determined by identifying the distance that the marker is to be spaced apart from the array to accurately measure the marker signal, and then arrange the coils so that the maximum dimension of the array is approximately 100% to 300% of that distance. The maximum dimension of thearray1605, for example, can be approximately 200% of the sensing distance at which a marker is to be placed from thearray1605. In one specific embodiment, themarker40 has a sensing distance of 20 cm and the maximum dimension of the array ofcoils1602 is between 20 cm and 60 cm, and more specifically 40 cm.
A coil array with a maximum dimension as set forth above is particularly useful because it inherently provides a filter that mitigates interference from far field sources. As such, one aspect of several embodiments of the invention is to size the array based upon the signal from the marker so that the array preferentially measures near field sources (i.e., the field generated by the marker) and filters interference from far field sources.
Thecoils1602 are electromagnetic field sensors that receive magnetic flux produced by thewireless markers40 and in turn produce a current signal representing or proportional to an amount or magnitude of a component of the magnetic field through an inner portion or area of each coil. The field component is also perpendicular to the plane of eachcoil1602. Each coil represents a separate channel, and thus each coil outputs signals to one of 32output ports1606. A preamplifier, described below, may be provided at eachoutput port1606. Placing preamplifiers (or impedance buffers) close to the coils minimizes capacitive loading on the coils, as described herein. Although not shown, thesensing unit1601 also includes conductive traces or conductive paths routing signals from eachcoil1602 to itscorresponding output port1606 to thereby define a separate channel. The ports in turn are coupled to aconnector1608 formed on thepanel1604 to which an appropriately configured plug and associated cable may be attached.
Thesensing unit1601 may also include an onboard memory or other circuitry, such as shown by electrically erasable programmable read-only memory (EEPROM)1610. TheEEPROM1610 may store manufacturing information such as a serial number, revision number, date of manufacture, and the like. TheEEPROM1610 may also store per-channel calibration data, as well as a record of run-time. The run-time will give an indication of the total radiation dose to which the array has been exposed, which can alert the system when a replacement sensing subsystem is required.
Although shown in one plane only, additional coils or electromagnetic field sensors may be arranged perpendicular to thepanel1604 to help determine a three-dimensional location of thewireless markers40. Adding coils or sensors in other dimensions could increase the total energy received from thewireless markers40, but the complexity of such an array would increase disproportionately. The inventors have found that three-dimensional coordinates of thewireless markers40 may be found using the planar array shown inFIG. 19A-B.
Implementing thesensor assembly1012 may involve several considerations. First, thecoils1602 may not be presented with an ideal open circuit. Instead, they may well be loaded by parasitic capacitance due largely to traces or conductive paths connecting thecoils1602 to the preamplifiers, as well as a damping network (described below) and an input impedance of the preamplifiers (although a low input impedance is preferred). These combined loads result in current flow when thecoils1602 link with a changing magnetic flux. Any onecoil1602, then, links magnetic flux not only from thewireless marker40, but also from all the other coils as well. These current flows should be accounted for in downstream signal processing.
A second consideration is the capacitive loading on thecoils1602. In general, it is desirable to minimize the capacitive loading on thecoils1602. Capacitive loading forms a resonant circuit with the coils themselves, which leads to excessive voltage overshoot when theexcitation source1010 is energized. Such a voltage overshoot should be limited or attenuated with a damping or “snubbing” network across thecoils1602. A greater capacitive loading requires a lower impedance damping network, which can result in substantial power dissipation and heating in the damping network.
Another consideration is to employ preamplifiers that are low noise. The preamplification can also be radiation tolerant because one application for thesensor assembly1012 is with radiation therapy systems that use linear accelerators (LINAC). As a result, PNP bipolar transistors and discrete elements may be preferred. Further, a DC coupled circuit may be preferred if good settling times cannot be achieved with an AC circuit or output, particularly if analog to digital converters are unable to handle wide swings in an AC output signal.
FIG. 20, for example, illustrates an embodiment of asnubbing network1702 having adifferential amplifier1704. Thesnubbing network1702 includes two pairs of series coupled resistors and a capacitor bridging therebetween. Abiasing circuit1706 allows for adjustment of the differential amplifier, while acalibration input1708 allows both input legs of the differential amplifier to be balanced. Thecoil1602 is coupled to an input of thedifferential amplifier1704, followed by a pair of highvoltage protection diodes1710. DC offset may be adjusted by a pair of resistors coupled to bases of the input transistors for the differential amplifier1704 (shown as having a zero value). Additional protection circuitry is provided, such asESD protection diodes1712 at the output, as well as filtering capacitors (shown as having a 10 nF value).
c. Signal Processors and Controllers
Thesignal processor1014 and thecontroller1016 illustrated inFIG. 10 receive the signals from thesensor assembly1012 and calculate the absolute positions of themarkers40 within the reference frame. Suitable signal processing systems and algorithms are set forth in U.S. application Ser. Nos. 10/679,801; 10/749,478; 10/750,456; 10/750,164; 10/750,165; 10/749,860; and 10/750,453, all of which are incorporated herein by reference.
EXAMPLE Overview
An experimental phantom based study was conducted to determine effectiveness of this system for real-time tracking. In this experiment, a custom 4D stage was constructed to allow arbitrary motion in three axes for speeds up to 10 cm/sec in each dimension, with accuracy to 0.3 mm. Position accuracy was measured by a 3D digitizing arm attached to the stage system. As shown inFIG. 21, two ellipses were created with peak to peak motion of 2 cm, 4 cm and 2 cm; and 1 cm by 2 cm and 1 cm in the x, y and z direction respectively. Three periods were used to correspond to 15, 17 and 20 breaths per minute. A single transponder was used with an integration time of 33 ms, 67 ms and 100 ms and two transponders were used with integration times of 67 ms and 100 ms. The transponders were placed in a custom phantom mounted to the 4D stage. The experiment was performed with the isocenter placed 14 cm from the AC magnetic array to simulate the position of an average lung cancer patient. The 4D stage ran each trajectory while the real time tracking system measured the transponder positions. Measured position was compared against the phantom position. The effects of ellipse size, speed, transponder number and integration time were characterized.
Experiment Summary
As shown inFIG. 22, the root mean square (RMS) error was less than 1 mm for each ellipse, period and transponder integration time. The system was able to track points throughout the path of the ellipse, for example, in a trajectory of a large ellipse moving at 17 breaths per minute.FIG. 23 is a histogram of localization errors illustrating that the range of error was low for each point measured. As shown inFIG. 24, the RMS error was higher in areas of increased velocity in most trajectories. With respect to this experiment, a single transponder system performed slightly better than dual transponder systems, with the best system being a single transponder with a 67 ms integration time.
CONCLUSION The above description of illustrated embodiments, including what is described in the Abstract, is not intended to be exhaustive or to limit the invention to the precise forms disclosed. Although specific embodiments of and examples are described herein for illustrative purposes, various equivalent modifications can be made without departing from the spirit and scope of the invention, as will be recognized by those skilled in the relevant art. The teachings provided herein of the invention can be applied to target locating and tracking systems, not necessarily the exemplary system generally described above.
The various embodiments described above can be combined to provide further embodiments. All of the U.S. patents, U.S. patent application publications, U.S. patent applications, foreign patents, foreign patent applications and non-patent publications referred to in this specification and/or listed in the Application Data Sheet, are incorporated herein by reference, in their entirety. Aspects of the invention can be modified, if necessary, to employ systems, devices and concepts of the various patents, applications and publications to provide yet further embodiments of the invention.
These and other changes can be made to the invention in light of the above-detailed description. In general, in the following claims, the terms used should not be construed to limit the invention to the specific embodiments disclosed in the specification and the claims, but should be construed to include all target locating and monitoring systems that operate in accordance with the claims to provide apparatus and methods for locating, monitoring, and/or tracking the position of a selected target within a body. Accordingly, the invention is not limited, except as by the appended claims.