CN108227740A - Aircraft chain rupture control method and aircraft - Google Patents
Aircraft chain rupture control method and aircraft Download PDFInfo
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- CN108227740A CN108227740A CN201711498516.3A CN201711498516A CN108227740A CN 108227740 A CN108227740 A CN 108227740A CN 201711498516 A CN201711498516 A CN 201711498516A CN 108227740 A CN108227740 A CN 108227740A
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- 238000000034 method Methods 0.000 title claims abstract description 43
- 238000004891 communication Methods 0.000 claims abstract description 65
- 230000033001 locomotion Effects 0.000 claims abstract description 10
- 230000006870 function Effects 0.000 claims description 19
- 238000012217 deletion Methods 0.000 claims description 7
- 230000037430 deletion Effects 0.000 claims description 7
- 230000004913 activation Effects 0.000 claims description 3
- 238000007667 floating Methods 0.000 claims description 3
- 230000008569 process Effects 0.000 description 6
- 238000005516 engineering process Methods 0.000 description 5
- 230000005540 biological transmission Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 206010000369 Accident Diseases 0.000 description 3
- 238000004458 analytical method Methods 0.000 description 3
- 238000003860 storage Methods 0.000 description 3
- 230000004888 barrier function Effects 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 238000010079 rubber tapping Methods 0.000 description 2
- 230000008054 signal transmission Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000003213 activating effect Effects 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 210000003128 head Anatomy 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 210000003733 optic disk Anatomy 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
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, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- 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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
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- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Closed-Circuit Television Systems (AREA)
Abstract
The embodiment of the invention discloses a kind of aircraft chain rupture control method and aircraft, belong to aircraft field, and this method includes：Obtain the communication link information between the aircraft and controller；Based on the communication link information, the link communication state of the aircraft is determined；When the aircraft is in chain rupture state, the recording function of the aircraft is opened；And in a state that the aircraft opens recording function, the holder of the aircraft is controlled according to default video recording regular motion.By the scheme of the application, the function of aircraft is improved.
Description
Technical field
The present invention relates to vehicle technology field more particularly to aircraft chain rupture control technologies.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft or fully or intermittently independently operated by car-mounted computer.Compared with manned aircraft, nobody
Machine can perform task in more dangerous or rugged environment.Unmanned plane press application field, can be divided into it is military with it is civilian.It is military
Aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+sector application are that unmanned plane has really just needed；At present
It taking photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, news
The application in report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, has greatly expanded the use of unmanned plane in itself
On the way.
More and more with the use of unmanned plane, usage scenario is more and more extensive, domestic at present for civilian legal wireless
Electric frequency range is just so several, and, all generally using the legal frequency range, causing to interfere with each other causes flight chain rupture out of hand for everybody, loses
The unmanned plane of control special hazard in the air falls down it is possible that phenomena such as pounding vehicle and people, Air Diary only have recorded aircraft therefore
Barrier problem, and no responsibility problem of hurting sb.'s feelings after aircraft bombing is obscured and can not be confirmed.
In view of the above-mentioned problems, there is an urgent need for a kind of completely new aircraft chain rupture control technologies.
Invention content
In view of this, the embodiment of the present invention provides a kind of aircraft chain rupture control method and aircraft, at least part of solution
Certainly problems of the prior art.
In a first aspect, an embodiment of the present invention provides a kind of aircraft chain rupture control method, including：
Obtain the communication link information between the aircraft and controller；
Based on the communication link information, the link communication state of the aircraft is determined；
When the aircraft is in chain rupture state, the recording function of the aircraft is opened；And
In a state that the aircraft opens recording function, the holder of the aircraft is controlled according to default video recording rule
Movement.
A kind of specific implementation according to embodiments of the present invention, it is described to obtain leading between the aircraft and controller
Believe link information, including：
Scan all signal frequency ranges of the aircraft；
Search in all signal frequency ranges whether the signal of communication of memory controller；
If in the presence of the signal of communication of the controller is read.
A kind of specific implementation according to embodiments of the present invention, it is described based on the communication link information, it determines described
The link communication state of aircraft, including：
Whether the turn-off time for judging the communication link between the aircraft and the controller is more than first threshold；
If so, determine that the aircraft is in chain rupture state.
A kind of specific implementation according to embodiments of the present invention, it is described based on the communication link information, it determines described
The link communication state of aircraft, including：
Whether the turn-off time for judging the communication link between the aircraft and the controller is more than second threshold；
If so, the aircraft is controlled to be in floating state, and control the aircraft in the first duration to the control
Device processed sends the connection signal of different frequency range；
If the aircraft is not received by the feedback signal of the controller in first duration, it is determined that described
Aircraft is in chain rupture state.
A kind of specific implementation according to embodiments of the present invention, it is described when the aircraft is in chain rupture state, it opens
The recording function of the aircraft is opened, including：
Judge the aircraft before chain rupture state whether in RECORD mode；
If the aircraft before chain rupture state in RECORD mode, when the aircraft is in chain rupture state after
The RECORD mode of the aircraft is held in continuation of insurance；
If the aircraft is not at RECORD mode before chain rupture state, the RECORD mode of the aircraft is opened.
A kind of specific implementation according to embodiments of the present invention, the method further include：
Whether judge the aircraft is in video recording halted state；
If so, closing the recording function of the aircraft, and the video file is cryptographically stored to flight
The default memory space of device.
A kind of specific implementation according to embodiments of the present invention, the method further include：
When the aircraft and the controller are in communication connection status, the video file is uploaded to service
Device.
A kind of specific implementation according to embodiments of the present invention, the method further include：
Judge whether the aircraft receives the deletion instruction for the video file；
When the aircraft receives the deletion instruction for the video file, user is prompted to input aircraft activation
Password.
A kind of specific implementation according to embodiments of the present invention, the holder of the control aircraft is according to default record
Picture regular motion, including：
Control the holder taken a crane shot or multi-angle ring clap.
Second aspect, the embodiment of the present invention additionally provide a kind of aircraft, including：
Communication antenna, the communication antenna transmitting or reception are for the signal of communication of controller；
Photographic device, the photographic device record the state of flight of the aircraft according to instruction；
Holder, the holder are connect with the photographic device, control the camera shooting posture of the photographic device；
Processor, the processor are communicated to connect with the communication antenna, the photographic device and the holder, are used for
Aircraft chain rupture control method described in execution aforementioned first aspect or any realization method of first aspect.
Aircraft chain rupture control method provided in an embodiment of the present invention and aircraft, when the aircraft is in chain rupture state
When, the recording function of the aircraft can be opened, and in a state that the aircraft opens recording function, control described fly
The holder of row device is according to default video recording regular motion.Aircraft can open security strategy after chain rupture is out of control as a result, utilize video recording
Pattern is recorded a video, and Video data is used for second-mission aircraft accident analysis, while Video data is for object responsibility of hurting sb.'s feelings after aircraft bombing
It determines.
Description of the drawings
It in order to illustrate the technical solution of the embodiments of the present invention more clearly, below will be to needed in the embodiment attached
Figure is briefly described, it should be apparent that, the accompanying drawings in the following description is only some embodiments of the present invention, for this field
For those of ordinary skill, without creative efforts, other attached drawings are can also be obtained according to these attached drawings.
Fig. 1 is a kind of aircraft chain rupture control flow schematic diagram provided in an embodiment of the present invention；
Fig. 2 is another aircraft chain rupture control flow schematic diagram provided in an embodiment of the present invention；
Fig. 3 is another aircraft chain rupture control flow schematic diagram provided in an embodiment of the present invention；
Fig. 4 is another aircraft chain rupture control flow schematic diagram provided in an embodiment of the present invention；
Fig. 5 is a kind of aircraft provided in an embodiment of the present invention and controller communication scheme.
Specific embodiment
The embodiment of the present invention is described in detail below in conjunction with the accompanying drawings.
It will be appreciated that described embodiment is only part of the embodiment of the present invention, instead of all the embodiments.Base
Embodiment in the present invention, those of ordinary skill in the art obtained without creative efforts it is all its
Its embodiment, shall fall within the protection scope of the present invention.
More and more with the use of unmanned plane, usage scenario is more and more extensive, domestic at present for civilian legal wireless
Electric frequency range is just so several, and, all generally using the legal frequency range, causing to interfere with each other causes flight chain rupture out of hand for everybody, loses
The unmanned plane of control special hazard in the air falls down it is possible that phenomena such as pounding vehicle and people, Air Diary only have recorded aircraft therefore
Barrier problem, and no responsibility problem of hurting sb.'s feelings after aircraft bombing is obscured and can not be confirmed.Aircraft opens another security strategy after chain rupture is out of control：It opens
Open RECORD mode；Video data is used for second-mission aircraft accident analysis, while Video data is true for object responsibility of hurting sb.'s feelings after aircraft bombing
It is fixed.
Referring to Fig. 1, an embodiment of the present invention provides a kind of aircraft chain rupture control methods, include the following steps：
S101 obtains the communication link information between the aircraft and controller.
By taking unmanned plane during flying device as an example, the signal of communication between usual unmanned plane and controller includes a plurality of types of letters
Number, for example, remote controller signal, data transfer signal, image transmitting signal.These signals can be by using for example wirelessly communicating
Chip is realized, in terms of data and image transmitting, WIFI transmission, analog signal transmission or the biography individually researched and developed may be used
Defeated hardware carries out signal transmission.WIFI can accomplish 600-800 meters or so of communication distance, in addition to this, can also pass through
The analog signal image transmission of 5.8G transmits hardware by designing specific image data, can ensure 1-2 kilometers of (reasons
Think environment 5km) reliable 720P high-definition images data transmission.Based on this, the processor of aircraft interior needs special monitoring to fly
Communication link information between row device and controller.
S102 based on the communication link information, determines the link communication state of the aircraft.
The communication protocol that different frequency range may be used between aircraft and controller communicates with controller, such as can be with
Wireless signal using the WIFI signal of 2.4G, the radio wave of low frequency or 72MHz etc. carries out communications.Using WIFI as
Example, WIFI data transmissions need transmitting terminal to initially set up communication handshake mechanism with receiving terminal, then transmit each size as 512 words
The data packet of section.In most cases, when occurring in signal interruption, WIFI needs to re-establish handshake mechanism.Pass through inquiry
Aircraft receives WIFI information, can determine whether the link communication state of aircraft is normal.
S103 when the aircraft is in chain rupture state, opens the recording function of the aircraft.
When between aircraft and controller when more than the regular hour (such as 10 seconds) communication connection can not be established, at this time
It can be assumed that aircraft is in chain rupture state.The recording function of unmanned plane can be opened at this time.
S104 in a state that the aircraft opens recording function, controls the holder of the aircraft according to default record
As regular motion.
Holder is carry moving camera or the equipment of other picture pick-up devices.Due to unmanned plane, angle passes through in flight course
It often changes, while motor rotation will also result in extremely strong high-frequency vibration, so needing an equipment to stablize camera lens to protect
Demonstrate,prove the stability of picture.Holder monitors the angle change of aircraft by sensors such as built-in gyroscopes, passes through motor band
The rotation of index glass head carrys out the inclination of Active Compensation angle, and camera lens is made to remain at a fixed angle.Holder and aircraft simultaneously
Connection using the damping devices such as shock-absorbing ball, the high-frequency vibration of motor generation can be filtered.
After the link of aircraft and controller disconnects, holder pitch axis can be controlled to go to and most taken a crane shot down, it can also
For tapping mode holder course and pitching movement in video process, multi-angle ring bat is carried out, records aircraft multi-angle position comprehensively
And environmental information.
The communication link information between the various ways acquisition aircraft and controller may be used.According to of the invention real
A kind of specific implementation of example is applied, referring to Fig. 2, the communication link information obtained between the aircraft and controller,
It can include：
S201 scans all signal frequency ranges of the aircraft.
Aircraft may be used multiple frequency range and receive the signal of controller, be supported at this time, it may be necessary to scan all aircraft
Signal frequency range.
S202, search in all signal frequency ranges whether the signal of communication of memory controller.
After the frequency range for knowing all supports of aircraft, it can be checked and accepted in these all band supports by antenna,
To judge whether the signal of communication of controller.
S203, if in the presence of the signal of communication of the controller is read.
Judge whether aircraft is in chain rupture state, various ways may be used to carry out, according to embodiments of the present invention
A kind of specific implementation, it is described based on the communication link information, it determines the link communication state of the aircraft, can wrap
It includes：
Whether S204 judges the turn-off time of communication link between the aircraft and the controller more than the first threshold
Value.
Due to flight environment of vehicle, flying distance or other communication interferences, lead between aircraft and controller
The situation of reconnection can be often generated, can monitor the link turn-off time between aircraft and controller whether more than the first threshold at this time
It is worth (for example, 10 seconds).
S205, if so, determining that the aircraft is in chain rupture state.
In addition to judging aircraft by the way of step S204-S205 whether other than the chain rupture state, referring to Fig. 3,
After step S203, other modes can also be used to be judged, a kind of specific implementation according to embodiments of the present invention,
It is described to be based on the communication link information, determine the link communication state of the aircraft, including：
Whether S301 judges the turn-off time of communication link between the aircraft and the controller more than the second threshold
Value.
S302 if so, the aircraft is controlled to be in floating state, and controls the aircraft in the first duration to institute
State the connection signal that controller sends different frequency range；
S303, judges whether the aircraft receives the feedback signal of the controller in first duration.
S304, if not, it is determined that the aircraft is in chain rupture state.
Other than aforesaid way, referring to Fig. 4, a kind of specific implementation according to embodiments of the present invention is described to work as institute
When stating aircraft and being in chain rupture state, the recording function of the aircraft is opened, including：
Judge the aircraft before chain rupture state whether in RECORD mode；
If the aircraft before chain rupture state in RECORD mode, when the aircraft is in chain rupture state after
The RECORD mode of the aircraft is held in continuation of insurance；
If the aircraft is not at RECORD mode before chain rupture state, the RECORD mode of the aircraft is opened.
Aircraft is by opening RECORD mode, and the state of flight being able to record after aircraft chain rupture is specific until reaching
State turn off recording function.A kind of specific implementation according to embodiments of the present invention, the method further include：
Whether judge the aircraft is in video recording halted state.Stop video recording or artificial closing electricity when generation is artificial
It is sent simultaneously during pond when halt instruction is shut down to aircraft camera or battery last work to low battery and sends stopping video recording simultaneously
When instructing to aircraft camera, it can be assumed that aircraft is in video recording halted state.
When aircraft is in video recording halted state, then the recording function of the aircraft is closed, and the video recording is literary
Part is cryptographically stored to the default memory space of aircraft.
For the ease of checking video file, alternatively, when the aircraft and the controller are in logical
When believing connection status, the video file is uploaded to server, such user can check clothes by modes such as mobile phone, computers
The video file being engaged on device.
Chain rupture video file belongs to encryption information file, can not arbitrarily delete, and deletion need to input aircraft activating pin, avoid
Passerby picks up aircraft person's malicious sabotage instrument of evidence.A kind of specific implementation according to embodiments of the present invention, the method is also
Including：
Judge whether the aircraft receives the deletion instruction for the video file；
When the aircraft receives the deletion instruction for the video file, user is prompted to input aircraft activation
Password.
Aircraft can control holder to record a video in several ways, a kind of specific implementation according to embodiments of the present invention
Mode, the holder of the control aircraft according to default video recording regular motion, including：
Control the holder taken a crane shot or multi-angle ring clap.After the link of aircraft and controller disconnects, it can control
Holder pitch axis, which is gone to, most to take a crane shot down, or tapping mode holder course and pitching movement in video process carry out
Multi-angle ring is clapped, and records aircraft multi-angle position and environmental information comprehensively.
Second aspect, referring to Fig. 5, the embodiment of the present invention additionally provides a kind of flight 1, including：
Communication antenna 101, the communication antenna 101 emit or receive the signal of communication for controller 2；
Photographic device 102, the photographic device 102 record the state of flight of the aircraft according to instruction；
Holder 103, the holder 103 are connect with the photographic device 102, control the camera shooting appearance of the photographic device 102
State；
Processor 104, the processor 104 and the communication antenna 101, the photographic device 102 and the holder
103 communication connections, for performing the aircraft chain rupture control method described in previous embodiment.
Aircraft chain rupture control method provided in an embodiment of the present invention and aircraft, when the aircraft is in chain rupture state
When, the recording function of the aircraft can be opened, and in a state that the aircraft opens recording function, control described fly
The holder of row device is according to default video recording regular motion.Aircraft can open security strategy after chain rupture is out of control as a result, utilize video recording
Pattern is recorded a video, and Video data is used for second-mission aircraft accident analysis, while Video data is for object responsibility of hurting sb.'s feelings after aircraft bombing
It determines.
It should be noted that herein, relational terms such as first and second and the like be used merely to by
One entity or operation are distinguished with another entity or operation, without necessarily requiring or implying these.
There are any actual relationship or orders between entity or operation.Moreover, term " comprising ", "comprising" or
Any other variant thereof is intended to cover non-exclusive inclusion by person, so that process, method, article including a series of elements
Or equipment not only includes those elements, but also including other elements that are not explicitly listed or to further include be this
Process, method, article or the intrinsic element of equipment.In the absence of more restrictions, by sentence " including one
It is a ... " limit element, it is not excluded that in the process, method, article or apparatus that includes the element also exist in addition
Identical element.
Each embodiment in this specification is described using relevant mode, identical similar portion between each embodiment
Point just to refer each other, and the highlights of each of the examples are difference from other examples.
For device embodiment, since it is substantially similar to embodiment of the method, so the comparison of description is simple
Single, the relevent part can refer to the partial explaination of embodiments of method.
Expression or logic and/or step described otherwise above herein in flow charts, for example, being considered use
In the order list for the executable instruction for realizing logic function, may be embodied in any computer-readable medium, for
Instruction execution system, device or equipment (such as computer based system, including the system of processor or other can be held from instruction
The system of row system, device or equipment instruction fetch and execute instruction) it uses or combines these instruction execution systems, device or set
It is standby and use.For the purpose of this specification, " computer-readable medium " can any can be included, store, communicate, propagate or pass
Defeated program is for instruction execution system, device or equipment or the dress used with reference to these instruction execution systems, device or equipment
It puts.The more specific example (non-exhaustive list) of computer-readable medium is including following：Electricity with one or more wiring
Connecting portion (electronic device), portable computer diskette box (magnetic device), random access memory (RAM), read-only memory
(ROM), erasable edit read-only storage (EPROM or flash memory), fiber device and portable optic disk is read-only deposits
Reservoir (CDROM).In addition, computer-readable medium can even is that the paper that can print described program on it or other are suitable
Medium, because can be for example by carrying out optical scanner to paper or other media, then into edlin, interpretation or when necessary with it
His suitable method is handled electronically to obtain described program, is then stored in computer storage.
It should be appreciated that each section of the present invention can be realized with hardware, software, firmware or combination thereof.
In the above-described embodiment, multiple steps or method can be with storages in memory and by suitably instructing execution
The software or firmware that system performs are realized.If for example, being realized with hardware in another embodiment, can use
Any one of following technology well known in the art or their combination are realized：With for data-signal realization logic work(
The discrete logic of the logic gates of energy has the application-specific integrated circuit of suitable combinational logic gate circuit, programmable gate
Array (PGA), field programmable gate array (FPGA) etc..
The above description is merely a specific embodiment, but protection scope of the present invention is not limited thereto, any
Those familiar with the art in the technical scope disclosed by the present invention, all should by the change or replacement that can be readily occurred in
It is included within the scope of the present invention.Therefore, protection scope of the present invention should be subject to the protection scope in claims.
Claims (10)
1. a kind of aircraft chain rupture control method, which is characterized in that including：
Obtain the communication link information between the aircraft and controller；
Based on the communication link information, the link communication state of the aircraft is determined；
When the aircraft is in chain rupture state, the recording function of the aircraft is opened；And
In a state that the aircraft opens recording function, the holder of the aircraft is controlled according to default video recording rule fortune
It is dynamic.
2. aircraft chain rupture control method according to claim 1, which is characterized in that described to obtain the aircraft and control
Communication link information between device processed, including：
Scan all signal frequency ranges of the aircraft；
Search in all signal frequency ranges whether the signal of communication of memory controller；
If in the presence of the signal of communication of the controller is read.
3. aircraft chain rupture control method according to claim 2, which is characterized in that described to be believed based on the communication link
Breath determines the link communication state of the aircraft, including：
Whether the turn-off time for judging the communication link between the aircraft and the controller is more than first threshold；
If so, determine that the aircraft is in chain rupture state.
4. aircraft chain rupture control method according to claim 2, which is characterized in that described to be believed based on the communication link
Breath determines the link communication state of the aircraft, including：
Whether the turn-off time for judging the communication link between the aircraft and the controller is more than second threshold；
If so, the aircraft is controlled to be in floating state, and control the aircraft in the first duration to the controller
Send the connection signal of different frequency range；
If the aircraft is not received by the feedback signal of the controller in first duration, it is determined that the flight
Device is in chain rupture state.
5. aircraft chain rupture control method according to claim 1, which is characterized in that described when the aircraft is in disconnected
During chain state, the recording function of the aircraft is opened, including：
Judge the aircraft before chain rupture state whether in RECORD mode；
If the aircraft is in RECORD mode before chain rupture state, when the aircraft is in chain rupture state after continuation of insurance
Hold the RECORD mode of the aircraft；
If the aircraft is not at RECORD mode before chain rupture state, the RECORD mode of the aircraft is opened.
6. aircraft chain rupture control method according to claim 5, which is characterized in that the method further includes：
Whether judge the aircraft is in video recording halted state；
If so, closing the recording function of the aircraft, and the video file is cryptographically stored to aircraft
Default memory space.
7. aircraft chain rupture control method according to claim 6, which is characterized in that the method further includes：
When the aircraft and the controller are in communication connection status, the video file is uploaded to server.
8. aircraft chain rupture control method according to claim 6, which is characterized in that the method further includes：
Judge whether the aircraft receives the deletion instruction for the video file；
When the aircraft receives the deletion instruction for the video file, user is prompted to input aircraft activation close
Code.
9. aircraft chain rupture control method according to claim 6, which is characterized in that the cloud of the control aircraft
Platform according to default video recording regular motion, including：
Control the holder taken a crane shot or multi-angle ring clap.
10. a kind of aircraft, which is characterized in that including：
Communication antenna, the communication antenna transmitting or reception are for the signal of communication of controller；
Photographic device, the photographic device record the state of flight of the aircraft according to instruction；
Holder, the holder are connect with the photographic device, control the camera shooting posture of the photographic device；
Processor, the processor is communicated to connect with the communication antenna, the photographic device and the holder, for performing
Aircraft chain rupture control method described in aforementioned any claim 1-9.
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| CN201711498516.3A CN108227740A (en) | 2017-12-29 | 2017-12-29 | Aircraft chain rupture control method and aircraft |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201711498516.3A CN108227740A (en) | 2017-12-29 | 2017-12-29 | Aircraft chain rupture control method and aircraft |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109714830A (en) * | 2019-01-09 | 2019-05-03 | 深圳市道通智能航空技术有限公司 | A kind of Air Diary method for uploading, device and mobile terminal, unmanned plane |
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| CN109714830A (en) * | 2019-01-09 | 2019-05-03 | 深圳市道通智能航空技术有限公司 | A kind of Air Diary method for uploading, device and mobile terminal, unmanned plane |
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