CN113677070B - Method, system, medium and application for controlling locking light treatment of formation aircraft - Google Patents
Method, system, medium and application for controlling locking light treatment of formation aircraft Download PDFInfo
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- CN113677070B CN113677070B CN202110968374.2A CN202110968374A CN113677070B CN 113677070 B CN113677070 B CN 113677070B CN 202110968374 A CN202110968374 A CN 202110968374A CN 113677070 B CN113677070 B CN 113677070B
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- 230000015572 biosynthetic process Effects 0.000 title claims abstract description 44
- 238000000034 method Methods 0.000 title claims abstract description 42
- 230000002159 abnormal effect Effects 0.000 claims abstract description 16
- 238000012545 processing Methods 0.000 claims abstract description 13
- 230000005856 abnormality Effects 0.000 claims abstract description 6
- 238000012546 transfer Methods 0.000 claims description 4
- 239000003086 colorant Substances 0.000 claims description 3
- 238000004590 computer program Methods 0.000 claims description 2
- 238000004886 process control Methods 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 8
- 230000006978 adaptation Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Classifications
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B47/00—Circuit arrangements for operating light sources in general, i.e. where the type of light source is not relevant
- H05B47/10—Controlling the light source
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B47/00—Circuit arrangements for operating light sources in general, i.e. where the type of light source is not relevant
- H05B47/10—Controlling the light source
- H05B47/165—Controlling the light source following a pre-assigned programmed sequence; Logic control [LC]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B20/00—Energy efficient lighting technologies, e.g. halogen lamps or gas discharge lamps
- Y02B20/40—Control techniques providing energy savings, e.g. smart controller or presence detection
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- Traffic Control Systems (AREA)
- Circuit Arrangement For Electric Light Sources In General (AREA)
Abstract
The application discloses a method, a system, a medium and an application for controlling locking light treatment of a formation aircraft, and relates to the technical field of unmanned aerial vehicles. In the flight process of the aircraft, a locking instruction is received, a locking instruction source is recorded, if the locking instruction comes from a background machine to control the aircraft to lock, a light-off instruction is sent only once, other operations are not carried out, the aircraft switches to an idle state, and a deviation light is sent by a deviation placing module according to the current position; if the locking reason is derived from the aircraft abnormality processing module, the light is turned off, the light interface mark is controlled, the light operation is not supported later, the aircraft is switched to an idle state, and the light failure is controlled by the placement deviation. According to the application, whether the lamplight is required to be permanently turned off is controlled by distinguishing the abnormal locking of the aircraft from the common locking control; the light is processed respectively, the effect of closing the aircraft light under the abnormal condition is achieved, and the technical effect that formation performance is not affected when part of aircraft is abnormal is guaranteed.
Description
Technical Field
The application belongs to the technical field of unmanned aerial vehicles, and particularly relates to a method, a system, a medium and application for controlling locking light treatment of a formation aircraft.
Background
In the formation performance industry, when the flight of an airplane is interfered during performance and emergency locking is needed to fall, the lamplight logic is abnormal, so that the demonstration picture is seriously influenced, the watching experience is seriously influenced, and if the lamp is directly turned off, the actual use is influenced when the airplane is locked on the ground at ordinary times.
At present, the light processing control logic of the formation aircraft is simultaneously controlled by a plurality of software task interfaces, and when abnormality occurs, the locking part can process the abnormality and turn off the light, so that the influence of the light on the formation performance pattern is prevented. However, the instructions for controlling the light by other tasks are still sent, the light can be turned on again, and then the light can be always bright in the falling process of the airplane, so that the performance effect cannot be guaranteed.
The design of the control method for the light treatment after locking the aircraft becomes the problem to be solved.
Through the above analysis, the problems and defects existing in the prior art are as follows: in the prior art, unmanned aerial vehicle dropped the in-process, light was always bright to formation aeronautical performance pattern interference, can not carry out a plurality of software task interfaces simultaneous control, had influenced normal show in the formation aeronautical performance pattern.
The meaning of solving the problems and the defects is as follows: the application solves the problem that unnecessary user impression loss is caused by the influence of uncertain light on the whole formation performance picture when the unmanned aerial vehicle is abnormally dropped in flight.
Disclosure of Invention
In order to overcome the problems in the related art, the disclosed embodiments of the application provide a method, a system, a medium and an application for controlling the locking light treatment of a formation aircraft. The technical scheme is as follows:
according to a first aspect of the disclosed embodiments of the present application, there is provided a method of controlling a locking light treatment of a formation aircraft, the method of controlling a locking light treatment of a formation aircraft comprising:
by distinguishing the abnormal locking of the aircraft from the normal locking control, whether the light control is handed over or not is controlled, so that the light turning-off can not be turned on by all light interfaces when the aircraft falls abnormally; after the background machine is controlled to lock, the normal flying aircraft still sends deviation light.
In an embodiment of the present application, the method for controlling locking light treatment of a formation aircraft specifically includes:
step one, in the flight process of an airplane, a locking instruction is received, and a locking instruction source is recorded;
step two, if the locking instruction comes from a background machine to control the aircraft to lock, executing step three, and if the locking reason comes from an aircraft exception handling module, skipping step three, and executing step four;
thirdly, the background machine only sends a lamp-turning-off instruction once and does not perform other operations;
and fourthly, when the light-off instruction of the background machine is from the aircraft abnormality processing module, the light interface in the aircraft is controlled to be turned off, the light processing interface is turned off, and the light control is not supported later.
In an embodiment of the present application, if the locking command is from the background machine, the aircraft switches from the state to the idle state, and the deviation module sends deviation light according to the current position.
In an embodiment of the application, the background machine further starts a placement deviation mode to judge that the placement deviation module is excessively large in deviation (within a range of one meter in horizontal distance), and for the condition of excessively large deviation, the lamplight can still be controlled and receive the instruction.
In an embodiment of the present application, in the fourth step, the aircraft switches to an idle state, the placement deviation controls the light to fail, and the light is still in the off mode.
In one embodiment of the application, after the aircraft is powered off and restarted, the first step to the fourth step are executed to control the aircraft locking light treatment.
According to a second aspect of the disclosed embodiments of the present application, there is provided a locking light treatment control system for a formation aircraft comprising:
the flight dancing step light control module is used for receiving locking instructions and recording the sources of the locking instructions in the flight process;
the background machine is connected with the flying dancing step light control module and is used for distinguishing abnormal locking and common locking control of the aircraft and controlling whether to transfer light control or not, so that when the aircraft falls abnormally, the light turning-off can not be turned on by all light interfaces any more;
the aircraft anomaly processing module is connected with the flying dance step light control module and is used for sending aircraft abnormal drop information to the flying dance step light control module;
the deviation module is connected with the flying dance step light control module and used for sending deviation light;
and the light control interface is connected with the flying dance step light control module and is used for connecting lamps with different colors.
According to a third aspect of the disclosed embodiments of the application, there is provided a computer readable storage medium storing a computer program which, when executed by a processor, causes the processor to perform a method of controlling the locking light treatment of a fleet aircraft.
According to a fourth aspect of the disclosed embodiments of the present application, there is provided a formation aircraft that performs a method of locking light treatment control of the formation aircraft.
According to a fifth aspect of the disclosed embodiments of the application, there is provided an application of a method for controlling the locking light treatment of a formation aircraft in the normal presentation of a formation aeronautical performance pattern.
The technical scheme provided by the embodiment of the application can comprise the following beneficial effects:
the application provides a light treatment control method after locking a formation aircraft, which is characterized in that a method for distinguishing flight abnormality locking from other locking modes and controlling whether to transfer light control rights is adopted, so that the light turning-off can not be turned on by all light interfaces any more when the aircraft falls abnormally, the function that the light can be restored after the background aircraft is locked is controlled, the problem of interference of the light on formation flight performance patterns in the falling process of the aircraft is solved, and the technical effect of normal display in the formation performance patterns is obtained.
Advantages of the present application compared to the prior art further include:
according to the application, whether the lamplight is required to be permanently turned off is controlled by distinguishing the abnormal locking of the aircraft from the common locking control; the light is processed respectively, the effect of closing the aircraft light under the abnormal condition is achieved, and the technical effect that formation performance is not affected when part of aircraft is abnormal is guaranteed.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the application as disclosed.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments consistent with the disclosure and together with the description, serve to explain the principles of the disclosure.
Fig. 1 is a flowchart of a method for controlling light treatment after locking a formation aircraft according to an embodiment of the present application.
Fig. 2 is a schematic diagram of a locking light processing control system for a formation aircraft according to an embodiment of the present application.
In the figure: 1. a flying dance step light control module; 2. a background machine; 3. an aircraft exception handling module; 4. placing a deviation module; 5. and a light control interface.
Fig. 3 is a schematic diagram showing that after the light priority is set to 4, no subsequent rgbw setting parameter is in operation according to the embodiment of the present application.
Detailed Description
Reference will now be made in detail to exemplary embodiments, examples of which are illustrated in the accompanying drawings. When the following description refers to the accompanying drawings, the same numbers in different drawings refer to the same or similar elements, unless otherwise indicated. The implementations described in the following exemplary examples are not representative of all implementations consistent with the present disclosure. Rather, they are merely examples of apparatus and methods consistent with some aspects of the present disclosure as detailed in the accompanying claims.
In the prior art, when a formation aircraft normally flies, lamplight is controlled by a dancing step module to send a waypoint.
When the formation aircraft flies idle, the light is controlled by the placement deviation module 4.
When the back office aircraft 2 controls the aircraft to lock, the lights are turned off once, but then the back office aircraft needs to be turned on normally.
When the formation aircraft flies abnormally, the locking module sends a once-off lamp, the follow-up lamp is not supported to be opened any more, and the aircraft lamp is opened to influence the performance effect in the process of abnormal aircraft falling caused by multitasking disorder.
Based on the problems existing in the prior art, the application provides a lamplight treatment control method after locking a formation aircraft. Comprising the following steps:
by distinguishing the abnormal locking of the aircraft from the normal locking control, whether the light control is handed over or not is controlled, so that the light turning-off can not be turned on by all light interfaces when the aircraft falls abnormally; after the background machine 2 is controlled to lock, the normal flying aircraft still sends deviation light.
Specifically, as shown in fig. 1, the method for controlling light treatment after locking of a formation aircraft provided by the embodiment of the application includes:
in the flight process of the aircraft, a locking instruction is received, a locking instruction source is recorded, if the locking instruction comes from the background machine 2 to control the locking of the aircraft, a lamp turning-off instruction is sent once, other operations are not carried out, the aircraft is switched to an idle state, a deviation light is sent by the deviation module 4 according to the current position, whether the deviation is overlarge or not is judged, the light can still be controlled, and the instruction is received;
if the locking reason is derived from the aircraft anomaly processing module 3, the light is turned off, the light interface mark is controlled, the light operation is not supported later, the aircraft is switched to an idle state, the placement deviation controls the light to fail, the light is still in a turned-off mode, and the light is not restarted when the power is cut off.
The technical scheme of the application is further described below with reference to specific embodiments.
Examples
The method for controlling the locking light treatment of the formation aircraft specifically comprises the following steps:
step one, in the flight process of an airplane, a locking instruction is received, and a locking instruction source is recorded;
step two, if the locking instruction comes from the background machine 2 to control the aircraft to lock, executing step three, and if the locking reason comes from the aircraft exception handling module 3, skipping step three, and executing step four;
step three, the background machine 2 only sends a lamp-turning-off instruction once and does not perform other operations;
and step four, when the light-off instruction is from the aircraft anomaly processing module 3, the background aircraft 2 controls the light to be turned off by the aircraft internal light interface, and turns off the light processing interface, so that the light control is not supported later.
In a preferred embodiment of the present application, if the locking command is from the background machine 2, the aircraft switches from the state to the idle state, and the deviation module 4 sends deviation light according to the current position.
In a preferred embodiment of the present application, the background machine 2 further opens the placement deviation mode to determine that the placement deviation module 4 has excessive deviation, and for the case of excessive deviation, the light can still be controlled and receive the instruction. The deviation is in the range of one meter from horizontal.
In a preferred embodiment of the present application, in the fourth step, the aircraft is switched to an idle state, the placement deviation controls the light to fail, and the light is still in the off mode.
In a preferred embodiment of the application, after the aircraft is powered off and restarted, the first step to the fourth step are executed to control the aircraft locking light treatment.
As shown in fig. 2, the present disclosure provides a locking light treatment control system for a formation aircraft, comprising:
the flying dance step light control module 1 is used for receiving locking instructions and recording the sources of the locking instructions in the flying process;
the background machine 2 is connected with the flying dance step light control module 1 and is used for distinguishing abnormal locking and common locking control of the aircraft, controlling whether to transfer light control or not, and realizing that the off light can not be turned on by all light interfaces when the aircraft falls abnormally;
the aircraft anomaly processing module 3 is connected with the flying dance step light control module 1 and is used for sending aircraft anomaly drop information to the flying dance step light control module 1;
the deviation placing module 4 is connected with the flying dance step light control module 1 and is used for sending deviation light;
and the light control interface 5 is connected with the flying dance step light control module 1 and is used for connecting lamps with different colors.
The effects of the present application are further described below in conjunction with experimental results.
As shown in fig. 3, after the light priority is set to 4, no subsequent rgb w setting parameters are active, in fig. 3, the horizontal axis is the time axis, and the vertical axis is the current aircraft running state and the light related parameters respectively.
Other embodiments of the disclosure will be apparent to those skilled in the art from consideration of the specification and practice of the disclosure disclosed herein. This application is intended to cover any adaptations, uses, or adaptations of the disclosure following, in general, the principles of the disclosure and including such departures from the present disclosure as come within known or customary practice within the art to which the disclosure pertains. It is intended that the specification and examples be considered as exemplary only, with a true scope and spirit of the disclosure being indicated by the following claims.
It is to be understood that the present disclosure is not limited to the precise arrangements and instrumentalities shown in the drawings, and that various modifications and changes may be effected without departing from the scope thereof. The scope of the present disclosure should be limited by the attached claims.
Claims (8)
1. A method of controlling a locking light treatment of a formation aircraft, the method comprising:
by distinguishing the abnormal locking of the aircraft from the normal locking control, whether the light control is handed over or not is controlled, so that the light turning-off can not be turned on by all light interfaces when the aircraft falls abnormally; after the background machine is controlled to lock, the normal flying aircraft still sends deviation light;
the method for controlling the locking light treatment of the formation aircraft specifically comprises the following steps:
step one, receiving a locking and turning-off instruction and recording a locking and turning-off instruction source in the flight process of an airplane;
step two, if the locking and turning-off instruction comes from a background machine to control the aircraft to lock and turn off the light, executing step three, and if the locking and turning-off instruction comes from an aircraft exception handling module, skipping step three, and executing step four;
thirdly, the background machine only sends a locking and turning-off instruction once and does not perform other operations;
and fourthly, when the locking and turning-off instruction is from the aircraft abnormality processing module, the internal light interface of the aircraft controls the light to be turned off, and the light processing interface is turned off, so that the light control is not supported later.
2. The method for controlling locking light treatment of formation aircraft according to claim 1, wherein if the locking light turning-off command is from a background aircraft, the aircraft switches state to idle state, and the deviation light is sent by the deviation module according to the current position.
3. The method for locking light process control of a fleet aircraft according to claim 1, wherein in the fourth step, the aircraft is switched to an idle state, the placement deviation control light is disabled, and the light remains in the off mode.
4. The method for controlling locking light treatment of a formation aircraft according to claim 1, wherein after the aircraft is powered off and restarted, the steps one to four are executed to perform locking light treatment control of the aircraft.
5. A formation aircraft locking light treatment control system implementing the method of formation aircraft locking light treatment control of any one of claims 1-4, the formation aircraft locking light treatment control system comprising:
the flying dance step light control module is used for receiving a locking and turning-off instruction and recording the source of the locking and turning-off instruction in the flying process;
the background machine is connected with the flying dancing step light control module and is used for distinguishing abnormal locking and common locking control of the aircraft and controlling whether to transfer light control or not, so that when the aircraft falls abnormally, the light turning-off can not be turned on by all light interfaces any more;
the aircraft anomaly processing module is connected with the flying dance step light control module and is used for sending aircraft abnormal drop information to the flying dance step light control module;
the deviation module is connected with the flying dance step light control module and used for sending deviation light;
and the light control interface is connected with the flying dance step light control module and is used for connecting lamps with different colors.
6. A computer readable storage medium storing a computer program which, when executed by a processor, causes the processor to perform the method of locking light treatment control of a enqueued aircraft as claimed in any one of claims 1 to 4.
7. A formation aircraft, characterized in that it performs a method of locking light treatment control of a formation aircraft according to any one of claims 1 to 4.
8. Use of a method for controlling the locking light treatment of a formation aircraft according to any one of claims 1 to 4 for the normal presentation of a formation aeronautical performance pattern.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202110968374.2A CN113677070B (en) | 2021-08-23 | 2021-08-23 | Method, system, medium and application for controlling locking light treatment of formation aircraft |
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| CN202110968374.2A CN113677070B (en) | 2021-08-23 | 2021-08-23 | Method, system, medium and application for controlling locking light treatment of formation aircraft |
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| CN113677070A CN113677070A (en) | 2021-11-19 |
| CN113677070B true CN113677070B (en) | 2023-10-31 |
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| CN113677070A (en) | 2021-11-19 |
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