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CN103050023B - Switching method for simultaneous display and control for multi-display ATC (Air Traffic Control) - Google Patents

Switching method for simultaneous display and control for multi-display ATC (Air Traffic Control)
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Publication number
CN103050023B
CN103050023BCN201210523884.XACN201210523884ACN103050023BCN 103050023 BCN103050023 BCN 103050023BCN 201210523884 ACN201210523884 ACN 201210523884ACN 103050023 BCN103050023 BCN 103050023B
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Prior art keywords
atc
display
mirror image
control
mode
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CN201210523884.XA
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CN103050023A (en
Inventor
王勇
王运盛
王蕾
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CETC Avionics Co Ltd
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CETC Avionics Co Ltd
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Abstract

The invention relates to the field of ATC (Air Traffic Control) and specifically discloses a switching method for simultaneous display and control for multi-display ATC. The switching method comprises a step of setting an ATC image driven mode corresponding to an ATC driving control mode. When an ATC operation is carried out by a display, the other displays in a same data link application enter into an ATC operation interface through the ATC image driven mode so as to carry out the ATC operation. According to the switching method for the simultaneous display and control for the multi-display ATC provided by the invention, a pilot can finish the switch of ATC display and control under the condition of ensuring safety, so that the driving risk of the pilot is reduced.

Description

Multi-display ATC shows simultaneously and controls changing method
Technical field
The present invention relates to air traffic control field, relate in particular to a kind of multi-display airway traffic control (ATC:Air Traffic Control) and show human-computer interactive control changing method.
Background technology
At present in Data-Link application air traffic control ATC, although there are multiple demonstration operating equipments (LEFTCDU10 and RIGHT CDU20) can be for ATC mutual (shown in Fig. 1), (only have a pilot and land station mutual for ensureing security, prevent from sending multiple requests or report simultaneously, cause the erroneous judgement of blank pipe), can only there is a pilot can operate ATC in some moment.In the time there is no equipment operating ATC, demonstration operating equipment 10 second row on the left side are shown as " <ATC ", show that ATC is enterable; And in the time of certain pilot's equipment operating ATC, on another pilot's display device, ATC is not enterable.In the time that pilot makes a forcible entry into ATC, system can show " IN USE, CHECK OTHER MCDU " similarly information.Only have in the time entering the equipment of ATC and exit ATC, other equipment just can enter ATC.
No doubt safety of above-mentioned this traditional design, but inconvenience brought, and pilot has complaint repeatly, has had airline to require the airborne ATC Human-computer Interactive Design of amendment, makes pilot can operate ATC simultaneously.By airline's investigation is learnt, the inconvenience that pilot denounces is that if captain does not exit ATC system, copilot cannot enter ATC system and check ground message in the time that captain's display device is just being received the message of ground management and control in ATC system.In the time of automatic flight, this situation can easily be processed, but when taking off or when the situation of the captain such as landing in busy state, the design that this captain of needs manually exits ATC system can make pilot divert one's attention, and brings flight risk.
Summary of the invention
The object of the invention is to, propose a kind of multi-display ATC and show simultaneously and control changing method, it can accomplish that in the situation that ensureing security a pilot can complete ATC and show the switching of controlling, and drives risk thereby reduce flight.
For achieving the above object, the invention provides a kind of multi-display ATC and show simultaneously and control changing method, it comprises: an ATC mirror image follower mode corresponding with ATC Active Control Mode is set; In the time having display operation ATC operation, enter ATC operation interface in other display of same Data-Link application by ATC mirror image follower mode, thereby carry out ATC operation.
In the present invention, also comprise before entering ATC operation interface by ATC mirror image follower mode described: step a, select to enter ATC interface, judge whether ATC has been presented at the step on other display, if be judged as NO, the display of current operation directly enters into ATC Active Control Mode; If be judged as YES, perform step b, the display of current operation enters ATC mirror image follower mode.
Further, after display enters ATC mirror image follower mode, also comprise and judge whether other display has exited the step of ATC operation, and if yes, the display of current operation directly enters into ATC Active Control Mode; If NO, perform step c, judge whether to obtain the control of ATC.
Wherein, described step c judges whether to obtain in the control of ATC, if be judged as NO, returns to step b, and the display of current operation enters ATC mirror image follower mode; If be judged as YES, confirm by controlling button, enter control conversion and confirm interface.
Moreover, described in enter control conversion and confirm also to comprise steps d behind interface, be confirmed whether to obtain ATC control, if NO, return to step b, the display of current operation enters ATC mirror image follower mode; If yes, after confirming, enter ATC Active Control Mode, thereby carry out ATC operation.
In the present invention, the core content that under described ATC mirror image follower mode, display shows is the same with the core content that display under ATC Active Control Mode shows.
Under ATC mirror image follower mode of the present invention, display can show ATC system information.
Multi-display ATC of the present invention shows simultaneously and controls changing method, it is by arranging ATC mirror image follower mode, can realize in airway traffic control multiple displays shows simultaneously and controls switching, even if main driving is opened ATC system, copilot also can enter ATC system and check ground message; Meanwhile, when taking off or when the situation of the captain such as landing in busy state, not needing main driving intervention can exit main ATC system yet, do not need the main driving copilot of diverting one's attention in ATC system, to operate, drive risk thereby reduce flight; In addition,, due to the setting of ATC mirror image follower mode, also can avoid the problem of ATC system deadlock.
Brief description of the drawings
In order to be illustrated more clearly in the embodiment of the present invention or technical scheme of the prior art, to the accompanying drawing of required use in embodiment or description of the Prior Art be briefly described below, apparently, accompanying drawing in the following describes is only some embodiments of the present invention, for those of ordinary skill in the art, do not paying under the prerequisite of creative work, can also obtain according to these accompanying drawings other accompanying drawing.
Fig. 1 is the schematic diagram of many display controls of airborne ATC in prior art;
Fig. 2 is the schematic flow sheet that multi-display ATC of the present invention shows simultaneously and control changing method.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is clearly and completely described, obviously, described embodiment is only the present invention's part embodiment, instead of whole embodiment.Based on the embodiment in the present invention, those of ordinary skill in the art, not making the every other embodiment obtaining under creative work prerequisite, belong to the scope of protection of the invention.
As shown in Figure 2, the invention provides a kind of multi-display ATC and show simultaneously and control changing method, it comprises: ATC mirror image driven (Slave) pattern corresponding with ATC active (Master) control model is set; In the time having display operation ATC operation, enter ATC operation interface in other display of same Data-Link application by ATC mirror image follower mode, thereby carry out ATC operation.Multi-display ATC of the present invention shows simultaneously and controls changing method, when it opens ATC system when main driving, copilot also can enter ATC system by mirror image follower mode and check ground message, when taking off or when the situation of the captain such as landing in busy state, do not need main driving manually to exit ATC system yet, can not make main driving divert one's attention, drive risk thereby reduce flight.
Concrete, in the present invention, also comprise before entering ATC operation interface by ATC mirror image follower mode described: step a, selection enters ATC interface, judge whether ATC has been presented at the step on other display, if be judged as NO, the display of current operation directly enters into ATC Active Control Mode; If be judged as YES, perform step b, the display of current operation enters ATC mirror image follower mode.In prior art, only have a pilot and land station mutual, in the time of certain pilot's equipment operating ATC, on another pilot's display device, ATC is not enterable, and in the inventive method, in the time finding that ATC does not show on other display device, can directly enter ATC Active Control Mode and operate; If while finding to have had ATC to show on other display device, can enter ATC mirror image follower mode and operate.Under this ATC mirror image follower mode, display can show ATC system information, and the shown core content of this display is the same with the core content that display under ATC Active Control Mode shows, but can not control, and can only browse.Highly ask interface as example taking ATC, the ATC of ATC Active Control Mode shows, can control and input character, control ATC mirror image follower mode, its core content is that ATC Active Control Mode is just the same, but can show " SL " in the first row, and show that be in ATC mirror image driven control model with prompting pilot " ATCMIRROR MODE " 5 seconds on note under.
Further, after display enters ATC mirror image follower mode, also comprise and judge whether other display has exited the step of ATC operation, and if yes, the display of current operation directly enters into ATC Active Control Mode; If NO, perform step c, judge whether to obtain the control of ATC.Wherein, judge whether to obtain in the control of ATC at described step c, if be judged as NO, return to step b, the display of current operation enters ATC mirror image follower mode; If be judged as YES, confirm by controlling button, enter control conversion and confirm interface.In the present invention, under ATC mirror image follower mode, if other display device exits ATC, ATC mirror image follower mode can automatically switch to ATC Active Control Mode.When other display device does not exit ATC yet, and the pilot of ATC mirror image follower mode wants to obtain the control of ATC, can take ATC operation effectively, for example, press the control button on display side, can enter ATC and control transition interface.If pilot presses cancellation (CANCEL) button, return to the original interface while entering ATC mirror image follower mode.
Moreover, described in enter control conversion and confirm also to comprise steps d behind interface, be confirmed whether to obtain ATC control, if NO, return to step b, the display of current operation enters ATC mirror image follower mode; If yes, after confirming, enter ATC Active Control Mode, thereby carry out ATC operation.In the specific embodiment of the invention, if pilot presses confirmation (VERIFY) button, can enter ATC Active Control Mode and return to original interface, ATC Active Control Mode originally switches to ATC mirror image follower mode, is presented switch prompting.
In sum, multi-display ATC of the present invention shows simultaneously and controls changing method, and it can not only can accomplish in the situation that ensureing security that a pilot can complete ATC and show the switching of controlling, and drives risk thereby reduce flight; Meanwhile, when in ATC system deadlock situation, it can be entered and be carried out release by ATC mirror image follower mode, thereby has solved the problem of original ATC system deadlock.
The foregoing is only preferred embodiment of the present invention, in order to limit the present invention, within the spirit and principles in the present invention not all, any amendment of doing, be equal to replacement, improvement etc., within all should being included in protection scope of the present invention.

Claims (6)

CN201210523884.XA2012-12-072012-12-07Switching method for simultaneous display and control for multi-display ATC (Air Traffic Control)ActiveCN103050023B (en)

Priority Applications (1)

Application NumberPriority DateFiling DateTitle
CN201210523884.XACN103050023B (en)2012-12-072012-12-07Switching method for simultaneous display and control for multi-display ATC (Air Traffic Control)

Applications Claiming Priority (1)

Application NumberPriority DateFiling DateTitle
CN201210523884.XACN103050023B (en)2012-12-072012-12-07Switching method for simultaneous display and control for multi-display ATC (Air Traffic Control)

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CN103050023Btrue CN103050023B (en)2014-10-29

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Citations (4)

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Publication numberPriority datePublication dateAssigneeTitle
CN101019004A (en)*2004-03-312007-08-15波音公司 Method and system for controlling the display of information on an aircraft cockpit
CN101093617A (en)*2006-06-232007-12-26莱斯莉·杰·莱内尔 safe lander
CN101201870A (en)*2007-12-202008-06-18四川川大智胜软件股份有限公司Method for dynamic simulation of air traffic flight posture
CN102456275A (en)*2010-10-262012-05-16霍尼韦尔国际公司Systems and methods for improving an in-trail procedures request

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* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US20030006910A1 (en)*2001-07-062003-01-09Dame Stephen G.Aural/visual interactive aircraft communications module, system and methods
GB0613054D0 (en)*2006-06-302006-08-09Nats En Route PlcAir traffic control

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* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CN101019004A (en)*2004-03-312007-08-15波音公司 Method and system for controlling the display of information on an aircraft cockpit
CN101093617A (en)*2006-06-232007-12-26莱斯莉·杰·莱内尔 safe lander
CN101201870A (en)*2007-12-202008-06-18四川川大智胜软件股份有限公司Method for dynamic simulation of air traffic flight posture
CN102456275A (en)*2010-10-262012-05-16霍尼韦尔国际公司Systems and methods for improving an in-trail procedures request

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