CN110329527A - A kind of UAV system with parachute safety guard - Google Patents
A kind of UAV system with parachute safety guard Download PDFInfo
- Publication number
- CN110329527A CN110329527A CN201910713524.8A CN201910713524A CN110329527A CN 110329527 A CN110329527 A CN 110329527A CN 201910713524 A CN201910713524 A CN 201910713524A CN 110329527 A CN110329527 A CN 110329527A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- module
- safety guard
- parachute
- uav system
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/40—Packs
- B64D17/52—Opening, e.g. manual
- B64D17/54—Opening, e.g. manual automatic
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S17/00—Systems using the reflection or reradiation of electromagnetic waves other than radio waves, e.g. lidar systems
- G01S17/88—Lidar systems specially adapted for specific applications
- G01S17/93—Lidar systems specially adapted for specific applications for anti-collision purposes
- G01S17/933—Lidar systems specially adapted for specific applications for anti-collision purposes of aircraft or spacecraft
-
- 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
- G05D1/104—Simultaneous control of position or course in three dimensions specially adapted for aircraft involving a plurality of aircrafts, e.g. formation flying
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06T—IMAGE DATA PROCESSING OR GENERATION, IN GENERAL
- G06T17/00—Three dimensional [3D] modelling, e.g. data description of 3D objects
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04W—WIRELESS COMMUNICATION NETWORKS
- H04W4/00—Services specially adapted for wireless communication networks; Facilities therefor
- H04W4/30—Services specially adapted for particular environments, situations or purposes
- H04W4/40—Services specially adapted for particular environments, situations or purposes for vehicles, e.g. vehicle-to-pedestrians [V2P]
- H04W4/44—Services specially adapted for particular environments, situations or purposes for vehicles, e.g. vehicle-to-pedestrians [V2P] for communication between vehicles and infrastructures, e.g. vehicle-to-cloud [V2C] or vehicle-to-home [V2H]
Abstract
The invention discloses a kind of UAV system with parachute safety guard; it include: unmanned plane, microprocessor, laser radar, parachute safety guard, ground base station and intelligent airplane parking area; the microprocessor is electrically connected with unmanned plane, laser radar and parachute safety guard respectively, the ground base station respectively with unmanned plane, intelligent airplane parking area communication connection.The present invention realizes the environment sensing of unmanned plane, the obstacle information around unmanned plane is effectively grasped, improve the avoidance effect of UAV system, reduce operation difficulty, improve the control precision of unmanned plane, it can prevent landing shock load from causing to damage to unmanned aerial vehicle body structure and airborne equipment, extend unmanned plane service life, ensure that UAV system can be reused, it can provide unmanned plane precisely to land, recharging, reduce the participation of Field Force, greatly improve products application efficiency, and it can realize unmanned plane clustered control, greatly improve unmanned plane work capacity.
Description
Technical field
The invention belongs to air vehicle technique fields, more specifically, more particularly to it is a kind of with parachute safeguard protection dress
The UAV system set.
Background technique
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 automatically operated by car-mounted computer.Compared with manned aircraft, nobody
Machine is often more suitable for the task of those too " slow-witted, dirty or dangerous ".Unmanned plane press application field, can be divided into it is military with it is civilian.
Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+industrial application are that unmanned plane has really just needed；
At present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping,
The application in news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, has greatly expanded unmanned plane itself
Purposes.
Automatic charging, the cluster mode of existing UAV system are still the problem for limiting the extensive operation of unmanned plane,
Its advantage can not be effectively played, and the barrier in flight path can not be detected and be evaded, therefore causes collision, pendant
Machine, since current unmanned plane cost is very high, collision or air crash accident can greatly increase the cost of user, at the same at present nobody
Application has been obtained in the parachute protective device of machine, but user must be manually operated parachute control button or carry out it
It operates and can release a parachute, and parachute defencive function receives restriction.
Therefore, it is proposed that a kind of UAV system with parachute safety guard.
Summary of the invention
The purpose of the present invention is to solve disadvantages existing in the prior art, realize the environment sensing of unmanned plane, have
The obstacle information of effect grasped around unmanned plane, improves the avoidance effect of UAV system, reduces operation difficulty, mention
The control precision of high unmanned plane, can prevent landing shock load from causing to damage to unmanned aerial vehicle body structure and airborne equipment, extend
Unmanned plane service life ensures that UAV system can be reused, it is possible to provide unmanned plane precisely land, recharging, reduction
The participation of Field Force greatly improves products application efficiency, and can realize unmanned plane clustered control, greatly improves unmanned machine operation
Ability, and a kind of UAV system with parachute safety guard proposed.
To achieve the above object, the invention provides the following technical scheme:
A kind of UAV system with parachute safety guard, comprising: unmanned plane, microprocessor, laser radar, landing
The inside of unmanned plane, the laser thunder is arranged in umbrella safety guard, ground base station and intelligent airplane parking area, the microprocessor
Up to being arranged on unmanned plane, the parachute safety guard is arranged in the top of unmanned plane, the microprocessor respectively with
Unmanned plane, laser radar and parachute safety guard are electrically connected, and the ground base station is shut down with unmanned plane, intelligence respectively
Level ground communication connection；
The microprocessor include laser radar drive module, three-dimension modeling module, automatic obstacle avoidance module, navigation module and
Flight control modules；
Laser radar driver built in the laser radar drive module, for controlling laser radar to unmanned plane ambient enviroment
360 ° of scannings are carried out, the ambient enviroment point cloud data of unmanned plane is obtained；
Environmental modeling program built in the three-dimension modeling module passes through a cloud for subscribing to ambient enviroment point cloud data
Digital three-dimensional model is generated with algorithm, and digital three-dimensional model is wirelessly transmitted to ground base station, with real-time display；
Avoidance program built in the automatic obstacle avoidance module for subscribing to ambient enviroment point cloud data, and calculates preset range cataract or glaucoma
Hinder object at a distance from unmanned plane and angle, according to distance and angle, determines current flight route；
Navigator built in the navigation module for obtaining current flight route, and calculates the current control parameter of unmanned plane；
The built-in flight control program of the flight control modules, for obtaining current control parameter, and generates current control instruction,
To control unmanned plane according to current flight route running；
The parachute safety guard includes sensor module, parachute, servo release module；
The sensor module is used to detect the state of flight of unmanned plane, and the state of flight for the unmanned plane that will acquire be sent to it is micro-
Processor；
The servo release module is used in the control unlatching parachute when unmanned plane lands.
Preferably, the intelligent airplane parking area includes shutting down platform, environment monitoring module, remote control module and automatic charging
Module, the environment monitoring module and automatic charging module pass through remote control module and ground base station communication connection respectively；
The environment monitoring module is used to detect the environment of the landing place of unmanned plane；
The automatic charging module is used to carry out automatic charging to unmanned plane after the completion of unmanned plane landing.
Preferably, the automatic charging module includes battery equilibrium protector and charging terminal, the charging terminal and
Battery equilibrium protector is coupled with remote control module, and the charging terminal matches with the charging port on unmanned plane.
It preferably, further include air bag buffer, the air bag buffer includes inflator module and air bag, the inflation
Module and microprocessor are electrically connected, and the inflator module is connected by pipeline with air bag, and the air bag is arranged in unmanned plane
Bottom.
Preferably, the inflator module uses inert gas, and the air bag uses rubber utricule.
It preferably, further include power supply device, the power supply device includes battery module and power supply circuit module, the storage
Battery module and power supply circuit module are electrically connected, and the power supply circuit module and microprocessor are electrically connected, for being entire
System is powered.
Preferably, the power supply device further includes solar powered module, the solar powered module and battery mould
Block is electrically connected, and is stored in battery module for being converted solar energy into electrical energy by solar panel.
Preferably, GPS positioning device is additionally provided on the unmanned plane, the GPS positioning device is electrically connected at micro- place
Manage device.
Technical effect and advantage of the invention:
A kind of UAV system with parachute safety guard provided by the invention, the present invention is by microprocessor and swashs
The cooperation of optical radar, realizes the environment sensing of unmanned plane, has effectively grasped the obstacle information around unmanned plane, has improved
The avoidance effect of UAV system, reduces operation difficulty, improves the control precision of unmanned plane, passes through microprocessor and parachute
Safety guard can automatically open parachute when unmanned plane lands, and protect unmanned aerial vehicle body, prevent landing shock load pair
Unmanned aerial vehicle body structure and airborne equipment cause to damage, and extend unmanned plane service life, ensure that UAV system can repeat to make
With, by the cooperation of microprocessor, intelligent airplane parking area and ground base station provide unmanned plane precisely land, recharging, reduce and show
The participation of field personnel, greatly improves products application efficiency, and can realize unmanned plane clustered control, greatly improves unmanned machine operation energy
Power.
Detailed description of the invention
Fig. 1 is that a kind of module of the communication connection of UAV system with parachute safety guard of the invention is shown
It is intended to；
Fig. 2 is a kind of module signal of the electric connection of UAV system with parachute safety guard of the invention
Figure；
Fig. 3 is that a kind of parachute safety guard of UAV system with parachute safety guard of the invention is beaten
The flow diagram opened；
Fig. 4 is a kind of STM32F103C8T6 single-chip microcontroller of UAV system with parachute safety guard of the invention
And its peripheral circuit schematic diagram；
Fig. 5 is a kind of working principle mould of the laser radar of UAV system with parachute safety guard of the invention
Type schematic diagram.
Specific embodiment
In order to make the objectives, technical solutions, and advantages of the present invention clearer, below in conjunction with attached drawing and specific implementation
Example, the present invention will be described in further detail.It should be appreciated that specific embodiment described herein is only used to explain this hair
It is bright, it is not intended to limit the present invention.Based on the embodiments of the present invention, those of ordinary skill in the art are not making creativeness
Every other embodiment obtained, shall fall within the protection scope of the present invention under the premise of labour.
Fig. 1-5 is please referred to, the present invention provides a kind of UAV system with parachute safety guard, comprising: nothing
Man-machine, microprocessor, laser radar, parachute safety guard, ground base station and intelligent airplane parking area, the microprocessor are set
It sets in the inside of unmanned plane, the laser radar is arranged on unmanned plane, and the parachute safety guard is arranged at nobody
The top of machine, the microprocessor are electrically connected with unmanned plane, laser radar and parachute safety guard respectively, describedly
Face base station respectively with unmanned plane, intelligent airplane parking area communication connection；
The microprocessor include laser radar drive module, three-dimension modeling module, automatic obstacle avoidance module, navigation module and
Flight control modules；
Laser radar driver built in the laser radar drive module, for controlling laser radar to unmanned plane ambient enviroment
360 ° of scannings are carried out, the ambient enviroment point cloud data of unmanned plane is obtained；
Environmental modeling program built in the three-dimension modeling module passes through a cloud for subscribing to ambient enviroment point cloud data
Digital three-dimensional model is generated with algorithm, and digital three-dimensional model is wirelessly transmitted to ground base station, with real-time display；
Avoidance program built in the automatic obstacle avoidance module for subscribing to ambient enviroment point cloud data, and calculates preset range cataract or glaucoma
Hinder object at a distance from unmanned plane and angle, according to distance and angle, determines current flight route；
Navigator built in the navigation module for obtaining current flight route, and calculates the current control parameter of unmanned plane；
The built-in flight control program of the flight control modules, for obtaining current control parameter, and generates current control instruction,
To control unmanned plane according to current flight route running；
The parachute safety guard includes sensor module, parachute, servo release module；
The sensor module is used to detect the state of flight of unmanned plane, and the state of flight for the unmanned plane that will acquire be sent to it is micro-
Processor；
The servo release module is used in the control unlatching parachute when unmanned plane lands.
Specifically, the intelligence airplane parking area includes shutting down platform, environment monitoring module, remote control module and automatic charging
Module, the environment monitoring module and automatic charging module pass through remote control module and ground base station communication connection respectively；
The environment monitoring module is used to detect the environment of the landing place of unmanned plane；
The automatic charging module is used to carry out automatic charging to unmanned plane after the completion of unmanned plane landing.
Specifically, the automatic charging module includes battery equilibrium protector and charging terminal, the charging terminal and
Battery equilibrium protector is coupled with remote control module, and the charging terminal matches with the charging port on unmanned plane.
Specifically, further including air bag buffer, the air bag buffer includes inflator module and air bag, the inflation
Module and microprocessor are electrically connected, and the inflator module is connected by pipeline with air bag, and the air bag is arranged in unmanned plane
Bottom.
Specifically, the inflator module uses inert gas, the air bag uses rubber utricule.
Specifically, further including power supply device, the power supply device includes battery module and power supply circuit module, the storage
Battery module and power supply circuit module are electrically connected, and the power supply circuit module and microprocessor are electrically connected, for being entire
System is powered.
Specifically, the power supply device further includes solar powered module, the solar powered module and battery mould
Block is electrically connected, and is stored in battery module for being converted solar energy into electrical energy by solar panel.
Specifically, being additionally provided with GPS positioning device on the unmanned plane, the GPS positioning device is electrically connected at micro- place
Manage device.
In summary: a kind of UAV system with parachute safety guard provided by the invention, the present invention are logical
The cooperation for crossing microprocessor and laser radar, realizes the environment sensing of unmanned plane, has effectively grasped the barrier around unmanned plane
Hinder object information, improve the avoidance effect of UAV system, reduce operation difficulty, improves the control precision of unmanned plane, pass through
Microprocessor and parachute safety guard can automatically open parachute when unmanned plane lands, and protect unmanned aerial vehicle body, prevent
Only landing shock load causes to damage to unmanned aerial vehicle body structure and airborne equipment, extends unmanned plane service life, ensures nobody
Machine system can be reused, precisely landed by the cooperation offer unmanned plane of microprocessor, intelligent airplane parking area and ground base station,
Recharging reduces the participation of Field Force, greatly improves products application efficiency, and can realize unmanned plane clustered control, substantially
Improve unmanned plane work capacity.
Finally, it should be noted that the foregoing is only a preferred embodiment of the present invention, it is not intended to restrict the invention,
Although the present invention is described in detail referring to the foregoing embodiments, for those skilled in the art, still may be used
To modify the technical solutions described in the foregoing embodiments or equivalent replacement of some of the technical features,
All within the spirits and principles of the present invention, any modification, equivalent replacement, improvement and so on should be included in of the invention
Within protection scope.
Claims (9)
1. a kind of UAV system with parachute safety guard characterized by comprising unmanned plane, microprocessor,
Laser radar, parachute safety guard, ground base station and intelligent airplane parking area, the microprocessor are arranged in unmanned plane
Portion, the laser radar are arranged on unmanned plane, and the top of unmanned plane is arranged in the parachute safety guard, described micro-
Processor respectively with unmanned plane, laser radar and parachute safety guard be electrically connected, the ground base station respectively with nothing
Man-machine, intelligent airplane parking area communication connection；
The microprocessor include laser radar drive module, three-dimension modeling module, automatic obstacle avoidance module, navigation module and
Flight control modules；
Laser radar driver built in the laser radar drive module, for controlling laser radar to unmanned plane ambient enviroment
360 ° of scannings are carried out, the ambient enviroment point cloud data of unmanned plane is obtained；
Environmental modeling program built in the three-dimension modeling module passes through a cloud for subscribing to ambient enviroment point cloud data
Digital three-dimensional model is generated with algorithm, and digital three-dimensional model is wirelessly transmitted to ground base station, with real-time display；
Avoidance program built in the automatic obstacle avoidance module for subscribing to ambient enviroment point cloud data, and calculates preset range cataract or glaucoma
Hinder object at a distance from unmanned plane and angle, according to distance and angle, determines current flight route；
Navigator built in the navigation module for obtaining current flight route, and calculates the current control parameter of unmanned plane；
The built-in flight control program of the flight control modules, for obtaining current control parameter, and generates current control instruction,
To control unmanned plane according to current flight route running；
The parachute safety guard includes sensor module, parachute, servo release module；
The sensor module is used to detect the state of flight of unmanned plane, and the state of flight for the unmanned plane that will acquire be sent to it is micro-
Processor；
The servo release module is used in the control unlatching parachute when unmanned plane lands.
2. a kind of UAV system with parachute safety guard according to claim 1, it is characterised in that: institute
Stating intelligent airplane parking area includes shutting down platform, environment monitoring module, remote control module and automatic charging module, the environment prison
It surveys module and automatic charging module passes through remote control module and ground base station communication connection respectively；
The environment monitoring module is used to detect the environment of the landing place of unmanned plane；
The automatic charging module is used to carry out automatic charging to unmanned plane after the completion of unmanned plane landing.
3. a kind of UAV system with parachute safety guard according to claim 2, it is characterised in that: institute
The automatic charging module stated includes battery equilibrium protector and charging terminal, the charging terminal and battery equilibrium protector with
Remote control module coupling, the charging terminal match with the charging port on unmanned plane.
4. a kind of UAV system with parachute safety guard according to claim 1, it is characterised in that: also
Including air bag buffer, the air bag buffer includes inflator module and air bag, and the inflator module and microprocessor are electric
Property connection, the inflator module is connected by pipeline with air bag, and the bottom of unmanned plane is arranged in the air bag.
5. a kind of UAV system with parachute safety guard according to claim 4, it is characterised in that: institute
Inflator module is stated using inert gas, the air bag uses rubber utricule.
6. a kind of UAV system with parachute safety guard according to claim 1, it is characterised in that: also
Including power supply device, the power supply device includes battery module and power supply circuit module, the power supply circuit module and Wei Chu
It manages device to be electrically connected, the battery module and power supply circuit module are electrically connected, for being powered for whole system.
7. a kind of UAV system with parachute safety guard according to claim 6, it is characterised in that: institute
Stating power supply device further includes solar powered module, and the solar powered module and battery module are electrically connected, for leading to
It crosses solar panel and converts solar energy into electrical energy and be stored in battery module.
8. a kind of UAV system with parachute safety guard according to claim 1, it is characterised in that: institute
It states and is additionally provided with GPS positioning device on unmanned plane, the GPS positioning device is electrically connected at microprocessor.
9. a kind of UAV system with parachute safety guard according to claim 1, it is characterised in that: institute
Microprocessor is stated using STM32F103C8T6 single-chip microcontroller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910713524.8A CN110329527A (en) | 2019-08-02 | 2019-08-02 | A kind of UAV system with parachute safety guard |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910713524.8A CN110329527A (en) | 2019-08-02 | 2019-08-02 | A kind of UAV system with parachute safety guard |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110329527A true CN110329527A (en) | 2019-10-15 |
Family
ID=68148484
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910713524.8A Pending CN110329527A (en) | 2019-08-02 | 2019-08-02 | A kind of UAV system with parachute safety guard |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110329527A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110989682A (en) * | 2019-12-30 | 2020-04-10 | 福州大学 | Unmanned aerial vehicle accurate landing method based on single base station |
| CN111301702A (en) * | 2020-03-23 | 2020-06-19 | 南京诚朴无人机有限公司 | Environment surveys uses unmanned aerial vehicle's signal device |
| CN111361738A (en) * | 2020-03-18 | 2020-07-03 | 李秀英 | Floor unmanned aerial vehicle express delivery system |
| CN113184208A (en) * | 2021-04-28 | 2021-07-30 | 李承真 | Environment support system based on unmanned aerial vehicle and application method thereof |
| CN114063630A (en) * | 2021-11-26 | 2022-02-18 | 深圳草莓创新技术有限公司 | Control method with different obstacle avoidance priorities for improving obstacle avoidance function of unmanned aerial vehicle |
-
2019
- 2019-08-02 CN CN201910713524.8A patent/CN110329527A/en active Pending
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110989682A (en) * | 2019-12-30 | 2020-04-10 | 福州大学 | Unmanned aerial vehicle accurate landing method based on single base station |
| CN110989682B (en) * | 2019-12-30 | 2021-06-01 | 福州大学 | Unmanned aerial vehicle accurate landing method based on single base station |
| CN111361738A (en) * | 2020-03-18 | 2020-07-03 | 李秀英 | Floor unmanned aerial vehicle express delivery system |
| CN111301702A (en) * | 2020-03-23 | 2020-06-19 | 南京诚朴无人机有限公司 | Environment surveys uses unmanned aerial vehicle's signal device |
| CN111301702B (en) * | 2020-03-23 | 2023-09-12 | 佛山市迅科管道探测有限公司 | Unmanned aerial vehicle's for environmental survey signal device |
| CN113184208A (en) * | 2021-04-28 | 2021-07-30 | 李承真 | Environment support system based on unmanned aerial vehicle and application method thereof |
| CN114063630A (en) * | 2021-11-26 | 2022-02-18 | 深圳草莓创新技术有限公司 | Control method with different obstacle avoidance priorities for improving obstacle avoidance function of unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN110329527A (en) | A kind of UAV system with parachute safety guard | |
| CN106774427B (en) | Unmanned aerial vehicle-based water area automatic inspection system and method | |
| CN204822072U (en) | Many rotor unmanned aerial vehicle aircraft with function is reconnoitered in fire control | |
| CN106769241B (en) | Unmanned aerial vehicle for atmosphere sampling detection and toxic and harmful gas early warning monitoring | |
| CN107405527A (en) | Unmanned vehicle with detachable computing device | |
| CN106054903A (en) | Multi-rotor unmanned aerial vehicle self-adaptive landing method and system | |
| CN205691166U (en) | Toxic and harmful monitors based on four rotor wing unmanned aerial vehicles | |
| CN106970639A (en) | A kind of harbour outdoor scene monitoring system and method based on unmanned aerial vehicle platform | |
| CN106218873B (en) | A kind of anti-crash protection structure of unmanned plane | |
| CN107329487A (en) | A kind of unmanned plane and robot link job platform in the air | |
| CN206552252U (en) | Possesses the extraordinary unmanned plane of counter unmanned plane function | |
| CN106814752A (en) | A kind of round-the-clock City Surveillance System based on unmanned plane cluster | |
| WO2017080028A1 (en) | Unmanned aerial vehicle system for positioning source of nuclear radiation | |
| CN106101511A (en) | A kind of full-automatic unmanned machine system | |
| CN105786017A (en) | Photovoltaic power station survey, operation and maintenance system based on unmanned aerial vehicle | |
| CN106849224A (en) | A kind of unmanned plane is continued a journey system automatically | |
| CN207249489U (en) | A kind of unmanned plane and robot link job platform in the air | |
| CN211890820U (en) | Air-ground cooperative intelligent inspection robot | |
| CN108803633A (en) | A kind of unmanned plane low latitude monitoring system based on mobile communications network | |
| CN208314570U (en) | A kind of novel unmanned plane bridge machinery flight course planning system | |
| CN208000379U (en) | A kind of road enforcement system based on unmanned plane and robot technology | |
| CN112750303A (en) | Highway patrol is alert with unmanned aerial vehicle system | |
| CN210310919U (en) | Unmanned aerial vehicle system with parachute safety arrangement | |
| CN206494135U (en) | A kind of unmanned plane | |
| CN108062051A (en) | A kind of fly able multi-function robot of disaster field |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |