CN107992077A - Aircraft fault rescue method and device - Google Patents
Aircraft fault rescue method and device Download PDFInfo
- Publication number
- CN107992077A CN107992077A CN201711332702.XA CN201711332702A CN107992077A CN 107992077 A CN107992077 A CN 107992077A CN 201711332702 A CN201711332702 A CN 201711332702A CN 107992077 A CN107992077 A CN 107992077A
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- Prior art keywords
- aircraft
- rescue
- target
- target aircraft
- flight device
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Classifications
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B23/00—Testing or monitoring of control systems or parts thereof
- G05B23/02—Electric testing or monitoring
- G05B23/0205—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
- G05B23/0208—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterized by the configuration of the monitoring system
- G05B23/0213—Modular or universal configuration of the monitoring system, e.g. monitoring system having modules that may be combined to build monitoring program; monitoring system that can be applied to legacy systems; adaptable monitoring system; using different communication protocols
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B2219/00—Program-control systems
- G05B2219/20—Pc systems
- G05B2219/24—Pc safety
- G05B2219/24065—Real time diagnostics
Abstract
The disclosure is directed to aircraft fault rescue method and device.When this method is included in the target aircraft exception in definite aircraft group, rescue flight device is confirmed, the rescue flight device is the aircraft beyond target aircraft described in aircraft group；Confirm the failure cause of the target aircraft；According to the failure cause, rescue instruction is sent to the rescue flight device, the rescue instruction is used for rescue flight device and target aircraft is implemented to rescue for failure cause.In the technical solution, after aircraft breaks down, according to different failures, determine different rescue modes, so as to reach without manual recovery failure aircraft, the rescue flight device with group can help target aircraft automatically, prevent target aircraft from losing, improve user experience.
Description
Technical field
This disclosure relates to communication system, more particularly to aircraft fault rescue method and device.
Background technology
At present, UAV abbreviation unmanned plane, is to utilize radio robot and the presetting apparatus provided for oneself
The not manned vehicle manipulated.Unmanned plane is actually the general designation of unmanned vehicle, can be divided from technical standpoint definition
For：Unmanned fixed wing aircraft, unmanned VTOL aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aerocraft, nobody
Parasol etc..Compared with manned aircraft, there is small, low cost, easy to use, low to operational environment requirement, battlefield to give birth to for it
Deposit the advantages that ability is stronger.
The content of the invention
The embodiment of the present disclosure provides scheme aircraft fault rescue method and device.The technical solution is as follows：
According to the first aspect of the embodiment of the present disclosure, there is provided a kind of aircraft fault rescue method, the aircraft belong to
The aircraft group that multiple aircraft are formed, including：
When the target aircraft in determining aircraft group is abnormal, rescue flight device is confirmed, the rescue flight device is winged
Aircraft described in row device group beyond target aircraft；
Confirm the failure cause of the target aircraft；
According to the failure cause, rescue instruction is sent to the rescue flight device, the rescue instruction is used to rescue winged
Row device is implemented to rescue for failure cause to target aircraft.
The technical scheme provided by this disclosed embodiment can include the following benefits：After aircraft breaks down,
According to different failures, different rescue modes is determined, so as to reach without manual recovery failure aircraft, with the rescue of group
Aircraft can help target aircraft automatically, prevent target aircraft from losing, and improve user experience.
In one embodiment, the failure cause of target aircraft is communication system failure, and the rescue instruction includes：
The rescue flight device reception target aircraft follows signal；
The target aircraft is guided to fly.
In one embodiment, for the target aircraft when communicating lost contact with control system, automatic send follows letter
Number；
The rescue flight device reception target aircraft follows signal to include：
The rescue flight device opening signal search system, search target aircraft follows signal.
In one embodiment, the failure cause of target aircraft is flight system failure, and the rescue instruction includes：
Rescue flight device flies to target aircraft position；
Carry target aircraft.
In one embodiment, when the speed of falling of the target aircraft exceedes predetermined threshold value, overhead suspension is automatically turned on
Floating pattern, waits target aircraft rescue.
According to the second aspect of the embodiment of the present disclosure, there is provided a kind of aircraft fault rescue method, the aircraft belong to
The aircraft group that multiple aircraft are formed, for aircraft when communicating lost contact with control system, automatic send follows signal；Or fly
When the speed of falling of row device exceedes predetermined threshold value, air suspension pattern is automatically turned on, waits target aircraft rescue.
According to the third aspect of the embodiment of the present disclosure, there is provided a kind of aircraft fault rescue device, the aircraft belong to
The aircraft group that multiple aircraft are formed, including：
First determining module, for when the target aircraft in determining aircraft group is abnormal, confirming rescue flight device,
The rescue flight device is the aircraft beyond target aircraft described in aircraft group；
Second determining module, for confirming the failure cause of the target aircraft；
Sending module, for according to the failure cause, rescue instruction, the rescue to be sent to the rescue flight device
Instruction is used for rescue flight device and target aircraft is implemented to rescue for failure cause.
According to the fourth aspect of the embodiment of the present disclosure, there is provided a kind of aircraft fault rescue device, the aircraft belong to
The aircraft group that multiple aircraft are formed, including：
Second sending module, for when communicating lost contact with control system, automatic send to follow signal；
Module is waited, for when the speed of falling of the aircraft exceedes predetermined threshold value, automatically turning on air suspension mould
Formula, waits for rescue aircraft rescue.
According to a fifth aspect of the embodiments of the present disclosure, there is provided a kind of aircraft fault rescue device, including：
Processor；
For storing the memory of processor-executable instruction；
Wherein, the processor is configured as：
Obtain the system information with each aircraft in group；
According to the system information of each aircraft, aircraft and its system to break down is determined；
According to the aircraft to break down and its system, the rescue of aircraft broken down described in rescue is determined
Scheme.
According to the 6th of the embodiment of the present disclosure the aspect, there is provided a kind of aircraft fault rescue device, including：
Processor；
For storing the memory of processor-executable instruction；
Wherein, the processor is configured as：
When communicating lost contact with control system, automatic send follows signal；
Or when the speed of falling of the aircraft exceedes predetermined threshold value, air suspension pattern is automatically turned on, is waited for rescue
Aircraft is rescued.
It should be appreciated that the general description and following detailed description of the above are only exemplary and explanatory, not
The disclosure can be limited.
Brief description of the drawings
Attached drawing herein is merged in specification and forms the part of this specification, shows the reality for meeting the disclosure
Apply example, and be used for together with specification the principle for explaining the disclosure.
Fig. 1 is the flow chart of the aircraft fault rescue method according to an exemplary embodiment.
Fig. 2 is the flow chart of the aircraft fault rescue method according to an exemplary embodiment.
Fig. 3 is the flow chart of the aircraft fault rescue method according to an exemplary embodiment.
Fig. 4 is the block diagram of the aircraft fault rescue device according to an exemplary embodiment.
Fig. 5 is the block diagram of the aircraft fault rescue device according to an exemplary embodiment.
Fig. 6 is the block diagram of the aircraft fault rescue device according to an exemplary embodiment.
Fig. 7 is the block diagram of the aircraft fault rescue device according to an exemplary embodiment.
Fig. 8 is the block diagram of the aircraft fault rescue device according to an exemplary embodiment.
Embodiment
Here exemplary embodiment will be illustrated in detail, its example is illustrated in the accompanying drawings.Following description is related to
During attached drawing, unless otherwise indicated, the same numbers in different attached drawings represent the same or similar key element.Following exemplary is implemented
Embodiment described in example does not represent all embodiments consistent with the disclosure.On the contrary, they are only and such as institute
The example of the consistent apparatus and method of some aspects be described in detail in attached claims, the disclosure.
In correlation technique, aircraft needs to contact with ground center always in flight course, and therefore, aircraft flies
Row system and communication system are all extremely important for whole flight, if any system goes wrong, aircraft is possibly can not be complete
Into whole flight.
The technical solution that the embodiment of the present disclosure provides, is related to two sides：Ground control centre and aircraft, wherein, ground control
Center processed is used for and aircraft keeps communication, can be flown with vectored flight device, and what aircraft can be according to ground control centre will
Ask and fly, can also fly according to the route of setting.
Fig. 1 is a kind of flow chart of aircraft fault rescue method according to an exemplary embodiment, such as Fig. 1 institutes
Show, aircraft fault rescue method is used in aircraft fault rescue device, which is applied to the control of control fault rescue
System, aircraft belong to the aircraft group that multiple aircraft are formed, and this method may comprise steps of 101-103：
In a step 101, when the target aircraft in determining aircraft group is abnormal, rescue flight device is confirmed.
Here, aircraft group includes being carrying out can mutually communicate one group of aircraft of aerial mission, target flight
Device is the aircraft to break down in aircraft group, and rescue flight device is the aircraft beyond target aircraft in aircraft group.
Rescue flight device can be a nearest aircraft not broken down of distance objective aircraft, such to rescue
Aircraft is helped easy to the most fast target aircraft that searches, completes rescue.There is event for flight system in this rescue flight device
The situation of barrier, if situation occurs in the communication system of target aircraft, target aircraft can not just share the positional information of oneself
.
Rescue flight device can also be in advance and target aircraft sets rescue relation, i.e. a side breaks down, another
Implement rescue in side.Here it is possible to before flight, the correspondence between corresponding aircraft is set in aircraft group, this is right
Should be related to can be stored in control system, can also be stored in each aircraft, break down in this way, working as any aircraft,
Just there is corresponding aircraft to go to rescue, without search.
Rescue flight device can also be the aircraft that rescue is exclusively used in flight crew, and aircraft group can be divided in advance
Work, present situation condition when institute role is distributed for each aircraft.The mark of rescue flight device can be stored in each in advance
In aircraft, in this way, which aircraft is problematic, it is possible to directly send aid request to the rescue flight device；Rescue flight
The mark of device can also be stored in control system, if which Fetion device is problematic, rescue center can assign rescue flight
Device goes to rescue.
Rescue flight device can also be the aircraft for the same flight crew that target aircraft searches, and the mode of search can
In a manner of including junction service, picture charge pattern.Junction service mode can include bluetooth, WiFi realize it is logical between aircraft
Letter.
In a step 102, the failure cause of target aircraft is confirmed.
Failure cause includes two kinds, and one kind is that target aircraft can not fly, i.e., flight system goes wrong, Yi Zhongshi
Target aircraft can not communicate, i.e., communication system goes wrong.Failure cause is different, and rescue method is different.The present embodiment leads to
Letter system, which goes wrong, to be referred generally to target aircraft and can not communicate with control system.
In step 103, according to failure cause, rescue instruction is sent to rescue flight device.
Rescue instruction is used for rescue flight device and target aircraft is implemented to rescue for failure cause.
In one embodiment, as shown in Fig. 2, when the target aircraft in determining aircraft group is abnormal, in Fig. 1
Step 102, that is, confirm the failure cause of target aircraft, can include：
In step 1021, when not receiving the flying quality of target aircraft, determine that the failure of target aircraft is former
Because communication system failure.
In step 1022, when target aircraft quickly falls, the failure cause for determining target aircraft is for flight
System failure.
If the speed of falling of the flying quality characterization aircraft of target aircraft exceedes predetermined threshold value, it is believed that occur
Flight system failure.At the same time, when the flying quality of target aircraft includes characterizing the flight broken down of flight system
During failure code, it is believed that flight system failure occurs.
In one embodiment, the failure cause of target aircraft is communication system failure, and rescue instruction includes：Rescue
Aircraft reception target aircraft follows signal；Guiding target aircraft flight.
Signal is followed to be used to be matched target aircraft with rescue flight device, in this way, rescue flight device can draw
Lead matched target aircraft.Follow signal can matching somebody with somebody with this kind of short-distance transmissions such as Bluetooth pairing signal, WiFi connection signals
To signal.
Rescue flight device guiding target aircraft flight can include：Sent to target aircraft sending control system
Flying quality, for example, target aircraft can fly according to flying quality.
Rescue flight device guiding target aircraft flight can include：Refer to the flight of oneself is sent with target aircraft
Order, when rescue flight device performs a flight directive, target aircraft also performs corresponding flight directive.
Rescue flight device guiding target aircraft flight can also include：Target aircraft can pass through image trace
Rescue flight device is followed, so as to fulfill the guiding of rescue flight device.
In one embodiment, for target aircraft when communicating lost contact with control system, automatic send follows signal；Rescue
That helps aircraft reception target aircraft follows signal, can include：
Rescue flight device opening signal search system, search target aircraft follows signal.
By taking bluetooth as an example, rescue flight device opens the Bluetooth function of itself, searches for the Bluetooth signal of surrounding, when searching
One signal, judge the signal whether be target aircraft the signal that follows, here, follow signal to carry target and fly
The mark of row device, rescue flight device can just be matched according to mark.
In the present embodiment, target aircraft refers to work as control system to target aircraft in the lost contact that communicates with control system
After sending a control information, back information is not received in preset time period, just both communication lost contacts of explanation.
In one embodiment, the failure cause of target aircraft is flight system failure, and rescue instruction includes：
Rescue flight device flies to the position of target aircraft；Carry target aircraft.
Can be that target aircraft is sent to control system at the position, control system is then forwarded to rescue flight device, rescues
Helping aircraft could fly at the position.
In one embodiment, when the speed of falling of target aircraft exceedes predetermined threshold value, air suspension mould is automatically turned on
Formula, waits target aircraft rescue.
Air suspension pattern is the pattern for keeping suspending in the air, if the propeller of aircraft breaks down, then open
Open spare propeller to keep suspending, without performing the aerial mission of aircraft again, wait for rescue.
The present embodiment provides a kind of aircraft fault rescue method, aircraft fault rescue method is used for aircraft failure
Deliverance apparatus, the device are applied to the aircraft of rescue, which belongs to the aircraft group that multiple aircraft are formed,
This method can include：
For aircraft when communicating lost contact with control system, automatic send follows signal；Or, the speed of falling of aircraft surpasses
When crossing predetermined threshold value, air suspension pattern is automatically turned on, waits target aircraft rescue.
Here, if the time that aircraft can not receive the return system of control system transmission exceedes preset duration, then just
Illustrate both communication lost contacts.
Speed of falling is the decrease speed on vertical direction.If aircraft may in Crater face, target aircraft
It can damage, the occurrence of this is a kind of in order to prevent, aircraft needs to open air suspension pattern.Air suspension pattern
After unlatching, spare propeller is opened, keeps aircraft to suspend in the air.
Fig. 3 is a kind of flow chart of aircraft fault rescue method according to an exemplary embodiment, such as Fig. 3 institutes
Show, aircraft fault rescue method is used in aircraft fault rescue device, and aircraft belongs to the flight that multiple aircraft are formed
Device group, this method are applied to aircraft failure rescue system, which includes the ground control centre as control system, mesh
Mark aircraft and rescue flight device.This method may comprise steps of 201-207：
In step 201, ground control centre confirms rescue when the target aircraft in determining aircraft group is abnormal
Aircraft.
Rescue flight device is the aircraft beyond target aircraft in aircraft group.
In step 202, ground control centre confirms the failure cause of target aircraft.
In step 203, ground control centre sends rescue instruction according to failure cause to rescue flight device.
Rescue instruction is used for rescue flight device and target aircraft is implemented to rescue for failure cause.
In step 204, when the failure cause of target aircraft is communication system failure, rescue flight device is according to rescuing
Instruction unpack signals search system is helped, that searches for target aircraft follows signal.
In step 205, when rescue flight device, which receives, follows signal, guiding target aircraft flight.
In step 206, when the failure cause of target aircraft is flight system failure, rescue flight device is according to rescuing
Instruction is helped, is flown to the position of target aircraft.
Rescue instruction is included at the position of target aircraft.
In step 207, rescue flight device carries target aircraft.
Following is embodiment of the present disclosure, can be used for performing embodiments of the present disclosure.
Fig. 4 is a kind of block diagram of aircraft fault rescue device according to an exemplary embodiment, which can be with
Pass through being implemented in combination with as some or all of of electronic equipment for software, hardware or both.As shown in figure 4, the aircraft
Fault rescue device includes：
First determining module 301, for when the target aircraft in determining aircraft group is abnormal, confirming rescue flight
Device, the rescue flight device are the aircraft beyond target aircraft described in aircraft group；
Second determining module 302, for confirming the failure cause of the target aircraft；
Sending module 303, it is described to rescue for according to the failure cause, rescue instruction to be sent to the rescue flight device
Help instruction and be used for rescue flight device for failure cause to target aircraft implementation rescue.
In one embodiment, as shown in figure 5, the target aircraft in the aircraft group is determined is different
Chang Shi, the second determining module 302 include：
First determination sub-module 3021, it is described for when not receiving the flying quality of the target aircraft, determining
The failure cause of target aircraft is communication system failure；
Second determination sub-module 3022, for when the target aircraft quickly falls, determining the target aircraft
Failure cause be flight system failure.
In one embodiment, the failure cause of the target aircraft is communication system failure, the rescue instruction bag
Include：
The rescue flight device reception target aircraft follows signal；
The target aircraft is guided to fly.
In one embodiment, for the target aircraft when communicating lost contact with control system, automatic send follows letter
Number；
The rescue flight device reception target aircraft follows signal to include：
The rescue flight device opening signal search system, search target aircraft follows signal.
In one embodiment, the failure cause of the target aircraft is flight system failure, the rescue instruction bag
Include：
The rescue flight device flies to the position of the target aircraft；
Carry the target aircraft.
In one embodiment, when the speed of falling of the target aircraft exceedes predetermined threshold value, overhead suspension is automatically turned on
Floating pattern, waits target aircraft rescue.
According to the third aspect of the embodiment of the present disclosure, there is provided a kind of aircraft fault rescue device, including：
Processor；
For storing the memory of processor-executable instruction；
Wherein, processor is configured as：
When the target aircraft in determining aircraft group is abnormal, rescue flight device is confirmed, the rescue flight device is winged
Aircraft described in row device group beyond target aircraft；
Confirm the failure cause of the target aircraft；
According to the failure cause, rescue instruction is sent to the rescue flight device, the rescue instruction is used to rescue winged
Row device is implemented to rescue for failure cause to target aircraft.
Wherein, the processor is configured as：
When the target aircraft in the definite aircraft group is abnormal, the confirmation target aircraft
Failure cause includes：
When not receiving the flying quality of the target aircraft, the failure cause for determining the target aircraft is
Communication system failure；Or
When the target aircraft quickly falls, the failure cause for determining the target aircraft is flight system event
Barrier.
The failure cause of the target aircraft is communication system failure, and the rescue instruction includes：
The rescue flight device reception target aircraft follows signal；
The target aircraft is guided to fly.
For the target aircraft when communicating lost contact with control system, automatic send follows signal；
The rescue flight device reception target aircraft follows signal to include：
The rescue flight device opening signal search system, search target aircraft follows signal.
The failure cause of the target aircraft is flight system failure, and the rescue instruction includes：
The rescue flight device flies to the position of the target aircraft；
Carry the target aircraft.
When the speed of falling of the target aircraft exceedes predetermined threshold value, air suspension pattern is automatically turned on, waits target
Aircraft is rescued.
Fig. 6 is a kind of block diagram of aircraft fault rescue device according to an exemplary embodiment, which can be with
Pass through being implemented in combination with as some or all of of electronic equipment for software, hardware or both.As shown in fig. 6, the aircraft
Fault rescue device includes：
Second sending module 401, for when communicating lost contact with control system, automatic send to follow signal；
Module 402 is waited, for when the speed of falling of the aircraft exceedes predetermined threshold value, automatically turning on overhead suspension
Floating pattern, waits for rescue aircraft rescue.
According to the fourth aspect of the embodiment of the present disclosure, there is provided a kind of aircraft fault rescue device, including：
Processor；
For storing the memory of processor-executable instruction；
Wherein, processor is configured as：
When communicating lost contact with control system, automatic send follows signal；
Or when the speed of falling of the aircraft exceedes predetermined threshold value, air suspension pattern is automatically turned on, is waited for rescue
Aircraft is rescued.
On the device in above-described embodiment, wherein modules perform the concrete mode of operation in the related party
It is described in detail in the embodiment of method, explanation will be not set forth in detail herein.
Fig. 7 is a kind of block diagram for aircraft fault rescue device according to an exemplary embodiment, the device
Suitable for control system.For example, device 1700 may be provided as a server.Device 1700 includes processing component 1722, its
Further comprise one or more processors, and as the memory resource representated by memory 1732, can be by for storing
Manage the instruction of the execution of component 1722, such as application program.The application program stored in memory 1732 can include one or
It is more than one each correspond to the module of one group of instruction.In addition, processing component 1722 is configured as execute instruction, to hold
The row above method.
Device 1700 can also include a power supply module 1726 and be configured as the power management of executive device 1700, and one
A wired or wireless network interface 1750 is configured as device 1700 being connected to network, and input and output (I/O) interface
1758.Device 1700 can be operated based on the operating system for being stored in memory 1732, such as Windows ServerTM, Mac
OS XTM, UnixTM, LinuxTM, FreeBSDTM or similar.
A kind of non-transitorycomputer readable storage medium, when the instruction in the storage medium is by device 1700
When managing device execution so that device 1700 is able to carry out above-mentioned aircraft fault rescue method, the described method includes：
When the target aircraft in determining aircraft group is abnormal, rescue flight device is confirmed, the rescue flight device is winged
Aircraft described in row device group beyond target aircraft；
Confirm the failure cause of the target aircraft；
According to the failure cause, rescue instruction is sent to the rescue flight device, the rescue instruction is used to rescue winged
Row device is implemented to rescue for failure cause to target aircraft.
When the target aircraft in the definite aircraft group is abnormal, the confirmation target aircraft
Failure cause includes：
When not receiving the flying quality of the target aircraft, the failure cause for determining the target aircraft is
Communication system failure；Or
When the target aircraft quickly falls, the failure cause for determining the target aircraft is flight system event
Barrier.
The failure cause of the target aircraft is communication system failure, and the rescue instruction includes：
The rescue flight device reception target aircraft follows signal；
The target aircraft is guided to fly.
For the target aircraft when communicating lost contact with control system, automatic send follows signal；
The rescue flight device reception target aircraft follows signal to include：
The rescue flight device opening signal search system, search target aircraft follows signal.
The failure cause of the target aircraft is flight system failure, and the rescue instruction includes：
The rescue flight device flies to the position of the target aircraft；
Carry the target aircraft.
When the speed of falling of the target aircraft exceedes predetermined threshold value, air suspension pattern is automatically turned on, waits target
Aircraft is rescued.
Fig. 8 is a kind of block diagram for aircraft fault rescue device according to an exemplary embodiment, the device
Suitable for control system.Fig. 8 is a kind of block diagram for pattern recognition device according to an exemplary embodiment.For example,
Device 1900 may be provided as a server.Device 1900 includes processing component 1922, it further comprises one or more
Processor, and as the memory resource representated by memory 1932, can be by the finger of the execution of processing component 1922 for storing
Order, such as application program.The application program stored in memory 1932 can include each one or more correspondence
In
Device 1900 can also include a power supply module 1926 and be configured as the power management of executive device 1900, and one
A wired or wireless network interface 1950 is configured as device 1900 being connected to network, and input and output (I/O) interface
1958.Device 1900 can be operated based on the operating system for being stored in memory 1932, such as Windows ServerTM, Mac
OS XTM, UnixTM, LinuxTM, FreeBSDTM or similar.
A kind of non-transitorycomputer readable storage medium, when the instruction in the storage medium is by device 1900
When managing device execution so that device 1900 is able to carry out above-mentioned aircraft fault rescue method, the described method includes：
When communicating lost contact with control system, automatic send follows signal；
Or when the speed of falling of the aircraft exceedes predetermined threshold value, air suspension pattern is automatically turned on, is waited for rescue
Aircraft is rescued.
Those skilled in the art will readily occur to the disclosure after considering specification and putting into practice disclosure disclosed herein
Other embodiments.This application is intended to cover any variations, uses, or adaptations of the disclosure, these modifications, purposes
Or adaptive change follow the disclosure general principle and including the disclosure it is undocumented in the art it is known often
Knowledge or conventional techniques.Description and embodiments are considered only as exemplary, and the true scope and spirit of the disclosure are by following
Claim point out.
It should be appreciated that the present disclosure is not limited to the precise structures that have been described above and shown in the drawings, and
And various modifications and changes may be made without departing from the scope thereof.The scope of the present disclosure is only limited by appended claim.
Claims (13)
1. a kind of aircraft fault rescue method, the aircraft belongs to the aircraft group that multiple aircraft are formed, its feature exists
In, including：
When the target aircraft in determining aircraft group is abnormal, rescue flight device is confirmed, the rescue flight device is aircraft
Aircraft described in group beyond target aircraft；
Confirm the failure cause of the target aircraft；
According to the failure cause, rescue instruction is sent to the rescue flight device, the rescue instruction is used for rescue flight device
Target aircraft is implemented to rescue for failure cause.
2. according to the method described in claim 1, it is characterized in that, the target in the aircraft group is determined flies
When row device is abnormal, the failure cause for confirming target aircraft includes：
When not receiving the flying quality of the target aircraft, the failure cause for determining the target aircraft is communication system
System failure；Or
When the target aircraft quickly falls, the failure cause for determining the target aircraft is flight system failure.
3. according to the method described in claim 2, it is characterized in that, the failure cause of the target aircraft is communication system event
Barrier, the rescue instruction include：
The rescue flight device reception target aircraft follows signal；
The target aircraft is guided to fly.
4. according to the method described in claim 3, it is characterized in that, the target aircraft is in the lost contact that communicates with control system
When, automatic send follows signal；
The rescue flight device reception target aircraft follows signal to include：
The rescue flight device opening signal search system, search target aircraft follows signal.
5. according to the method described in claim 2, it is characterized in that, the failure cause of the target aircraft is flight system event
Barrier, the rescue instruction include：
The rescue flight device flies to the position of the target aircraft；
Carry the target aircraft.
6. according to the method described in claim 5, it is characterized in that, the speed of falling of the target aircraft exceedes predetermined threshold value
When, air suspension pattern is automatically turned on, waits target aircraft rescue.
7. a kind of aircraft fault rescue method, the aircraft belongs to the aircraft group that multiple aircraft are formed, its feature exists
In, including：
When communicating lost contact with control system, automatic send follows signal；
Or when the speed of falling of the aircraft exceedes predetermined threshold value, air suspension pattern is automatically turned on, waits for rescue flight
Device is rescued.
8. a kind of aircraft fault rescue device, it is characterised in that the aircraft belongs to the aircraft that multiple aircraft are formed
Group, including：
First determining module, it is described to rescue for when the target aircraft in determining aircraft group is abnormal, confirming rescue flight device
Aircraft is helped as the aircraft beyond target aircraft described in aircraft group；
Second determining module, for confirming the failure cause of the target aircraft；
First sending module, for according to the failure cause, sending rescue instruction to the rescue flight device, the rescue refers to
Order is used for rescue flight device and target aircraft is implemented to rescue for failure cause.
9. a kind of aircraft fault rescue device, it is characterised in that the aircraft belongs to the aircraft that multiple aircraft are formed
Group, it is characterised in that including：
Second sending module, for when communicating lost contact with control system, automatic send to follow signal；
Module is waited, for when the speed of falling of the aircraft exceedes predetermined threshold value, automatically turning on air suspension pattern, etc.
Treat that rescue flight device is rescued.
A kind of 10. aircraft fault rescue device, it is characterised in that including：
Processor；
For storing the memory of processor-executable instruction；
Wherein, the processor is configured as：
When the target aircraft in determining aircraft group is abnormal, rescue flight device is confirmed, the rescue flight device is aircraft
Aircraft described in group beyond target aircraft；
Confirm the failure cause of the target aircraft；
According to the failure cause, rescue instruction is sent to the rescue flight device, the rescue instruction is used for rescue flight device
Target aircraft is implemented to rescue for failure cause.
A kind of 11. aircraft fault rescue device, it is characterised in that including：
Processor；
For storing the memory of processor-executable instruction；
Wherein, the processor is configured as：
When communicating lost contact with control system, automatic send follows signal；
Or when the speed of falling of the aircraft exceedes predetermined threshold value, air suspension pattern is automatically turned on, waits for rescue flight
Device is rescued.
12. a kind of computer-readable recording medium, is stored thereon with computer program, it is characterised in that the program is by processor
The step of any one of claim 1-6 the method is realized during execution.
13. a kind of computer-readable recording medium, is stored thereon with computer program, it is characterised in that the program is by processor
The step of claim 7 the method is realized during execution.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711332702.XA CN107992077A (en) | 2017-12-13 | 2017-12-13 | Aircraft fault rescue method and device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711332702.XA CN107992077A (en) | 2017-12-13 | 2017-12-13 | Aircraft fault rescue method and device |
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| CN110197360A (en) * | 2019-07-29 | 2019-09-03 | 南京邮电大学 | A kind of logistics unmanned plane having rescue function makes a return voyage dispatching method |
| CN110377020A (en) * | 2018-09-19 | 2019-10-25 | 北京京东尚科信息技术有限公司 | The running method of unmanned equipment, device and system |
| CN110780318A (en) * | 2019-10-16 | 2020-02-11 | 一飞智控(天津)科技有限公司 | Rescue method and control method for flight device after GPS (global positioning system) signal is lost |
| CN110962669A (en) * | 2018-09-29 | 2020-04-07 | 比亚迪股份有限公司 | Unmanned aerial vehicle rescue method, device, medium, cloud server and rescue system |
| CN112925341A (en) * | 2021-01-19 | 2021-06-08 | 北京京东乾石科技有限公司 | Flight control method of aircraft, related aircraft and aircraft system |
| CN114348264A (en) * | 2022-01-29 | 2022-04-15 | 国家海洋环境预报中心 | Unmanned aerial vehicle search and rescue method and system based on marine environment |
| CN114423681A (en) * | 2019-09-20 | 2022-04-29 | 帕拉泽罗科技有限公司 | Damage mitigation for aircraft with deployable parachutes |
| CN116736892A (en) * | 2023-08-15 | 2023-09-12 | 中国兵器装备集团兵器装备研究所 | Method and system for mutual aid return of flight equipment |
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| CN110197360A (en) * | 2019-07-29 | 2019-09-03 | 南京邮电大学 | A kind of logistics unmanned plane having rescue function makes a return voyage dispatching method |
| CN114423681A (en) * | 2019-09-20 | 2022-04-29 | 帕拉泽罗科技有限公司 | Damage mitigation for aircraft with deployable parachutes |
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