CN207712312U - A kind of rotor wing unmanned aerial vehicle auxiliary landing device - Google Patents
A kind of rotor wing unmanned aerial vehicle auxiliary landing device Download PDFInfo
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- CN207712312U CN207712312U CN201721669210.5U CN201721669210U CN207712312U CN 207712312 U CN207712312 U CN 207712312U CN 201721669210 U CN201721669210 U CN 201721669210U CN 207712312 U CN207712312 U CN 207712312U
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Abstract
The utility model provides a kind of rotor wing unmanned aerial vehicle auxiliary landing device, is related to unmanned plane technical field of auxiliary equipment, includes the airplane parking area control terminal on airplane parking area and the unmanned aerial vehicle (UAV) control end inside unmanned plane.Airplane parking area control terminal includes：Airplane parking area controller, magnetic induction sensor and magnetic locking device.Unmanned aerial vehicle (UAV) control end includes：Unmanned aerial vehicle (UAV) control device, motor, roller bearing, rope and magnetic patch.The technical solution is matched by airplane parking area control terminal in device and unmanned aerial vehicle (UAV) control end; it realizes the steady safety of unmanned plane, fast and accurately land; alleviate the unmanned plane of the existing technology technical problem big in the platform landing difficulty of high-speed mobile; it ensure that the accuracy of unmanned plane landing place; the safety for improving landing realizes reliable landing of the unmanned plane on the platform of high-speed mobile.
Description
Technical field
The utility model is related to unmanned plane technical field of auxiliary equipment, more particularly, to a kind of rotor wing unmanned aerial vehicle auxiliary landing
Device.
Background technology
Rotor wing unmanned aerial vehicle requires to obtain widely in civilian and military field with its high flexibility and lower landing condition
Development and application.Classical gyroplane unmanned plane, such as multi-rotor unmanned aerial vehicle, single rotor unmanned helicopter and coaxial to turning nobody
Helicopter plays important role in solution environmental monitoring, sea pollution monitoring, geography information collection etc..Even if certainly
Today of dynamic flight control system increasingly maturation, such unmanned plane still restrict it in taking off for complex condition with landing
It is used in wider field.
During realizing the utility model, inventor has found that at least there are the following problems in the prior art：It is multiple at some
Under the conditions of miscellaneous, such as landing of taking off in sea mobile platform, mobile ground surface platform of jolting, the flight of such unmanned plane is controlled
System and controllers are still stern challenge.Traditionally, such unmanned plane is when automatic or manual operation is landed,
Simple sensor is based primarily upon on artificial vision or unmanned plane to control balance, under non-stable operating environment, people
Sight and single sensor be highly susceptible to interfere, unmanned gyroplane is easy to topple, gently then blade damage, it is heavy then
Motor and the important equipment of carrying are damaged, therefore, platform of the prior art there are unmanned plane in high-speed mobile drops
Fall difficult technical problem.
Utility model content
In view of this, the purpose of this utility model is to provide a kind of rotor wing unmanned aerial vehicle auxiliary landing device, it is existing to alleviate
There is the technical problem that unmanned plane existing for technology is big in the platform landing difficulty of high-speed mobile.
The utility model embodiment provides a kind of rotor wing unmanned aerial vehicle auxiliary landing device, includes on airplane parking area
Airplane parking area control terminal and the unmanned aerial vehicle (UAV) control end inside unmanned plane；
Airplane parking area control terminal and unmanned aerial vehicle (UAV) control end are connected separately with the first power supply and second source；
Airplane parking area control terminal includes：Airplane parking area controller, magnetic induction sensor and magnetic locking device；
Airplane parking area controller is connected with magnetic induction sensor and magnetic locking device respectively；
Airplane parking area controller receives falling signal, and generates induction enabling signal, magnetic induction sensor according to falling signal
Magnetic locking signal is generated according to induction enabling signal, magnetic locking device is locked according to magnetic locking signal enabling, generates lock
Tight status signal, and locking state signal is sent by airplane parking area controller；
Unmanned aerial vehicle (UAV) control end includes：Unmanned aerial vehicle (UAV) control device, motor, roller bearing, rope and magnetic patch；
Unmanned aerial vehicle (UAV) control device, which is connected to the motor, to be connect, and motor is connected with roller bearing, and the outside of roller bearing is wound with rope, and the one of rope
End is fixed on roller bearing, and the other end is fixed with magnetic patch；
Unmanned aerial vehicle (UAV) control device receives falling signal, and generates electric motor starting letter according to falling signal or locking state signal
Number, motor drives roller bearing to rotate according to electric motor starting signal, and adjusts the length of rope release.
Further, in the rotor wing unmanned aerial vehicle auxiliary landing device that the utility model embodiment provides, magnetic locking device
Including：Electromagnet, pressure sensor, control relay and third power supply；
Control relay is connected with electromagnet, pressure sensor and third power supply respectively；
Relay is controlled to be locked according to magnetic locking signal enabling electromagnet, pressure sensor generates locking state signal,
Locking state signal is sent to airplane parking area controller.
Further, in the rotor wing unmanned aerial vehicle auxiliary landing device that the utility model embodiment provides, electric motor starting signal
Including rotating forward release signal and reversion tightening signal；
Motor drives roller bearing to rotate forward according to release signal is rotated forward, and increases the length of rope release；
Motor drives roller bearing reversion according to reversion tightening signal, and reduces the length of rope release.
Further, the rotor wing unmanned aerial vehicle auxiliary landing device that the utility model embodiment provides further includes and unmanned plane
The position sensor that controller is connected；
Position sensor generates and sends motor braking signal according to the position of magnetic patch；
Motor is braked according to motor braking signal.
The utility model embodiment brings following advantageous effect：The rotor wing unmanned aerial vehicle that the utility model embodiment is provided
Auxiliary landing device includes the airplane parking area control terminal on airplane parking area and the unmanned aerial vehicle (UAV) control inside unmanned plane
End.Airplane parking area control terminal and unmanned aerial vehicle (UAV) control end are connected separately with the first power supply and second source.Airplane parking area control terminal includes：Stop
Machine level ground controller, magnetic induction sensor and magnetic locking device.Airplane parking area controller respectively with magnetic induction sensor and magnetic key operated lock
Tight device is connected.Airplane parking area controller receives falling signal, and generates induction enabling signal according to falling signal, and magnetic induction passes
Sensor generates magnetic locking signal according to induction enabling signal, and magnetic locking device is locked according to magnetic locking signal enabling, raw
Locking state signal is sent at locking state signal, and by airplane parking area controller.Unmanned aerial vehicle (UAV) control end includes：Unmanned aerial vehicle (UAV) control
Device, motor, roller bearing, rope and magnetic patch.Unmanned aerial vehicle (UAV) control device, which is connected to the motor, to be connect, and motor is connected with roller bearing, the outside of roller bearing
It is wound with rope, one end of rope is fixed on roller bearing, and the other end is fixed with magnetic patch.Unmanned aerial vehicle (UAV) control device receives falling signal, and
Electric motor starting signal is generated according to falling signal or locking state signal, motor drives roller bearing to rotate according to electric motor starting signal,
And adjust the length of rope release.The technical solution is matched by airplane parking area control terminal in device and unmanned aerial vehicle (UAV) control end, real
Show the steady safety of unmanned plane, fast and accurately landed, while ensure that the accuracy of unmanned plane landing place, accelerates nothing
Man-machine sinking speed reduces the interference in unmanned plane descent, improves the safety of landing, realizes unmanned plane and exists
Reliable landing on the platform of high-speed mobile avoids the gyroplane occurred due to controlling balance because of vision or simple sensor and inclines
It covers, reduces the landing difficulty of unmanned plane, land in the platform of high-speed mobile to alleviate unmanned plane of the existing technology
The big technical problem of difficulty.
To enable the above objects, features, and advantages of the utility model to be clearer and more comprehensible, preferred embodiment cited below particularly, and
The appended attached drawing of cooperation, is described in detail below.
Description of the drawings
It, below will be right in order to illustrate more clearly of specific embodiment of the present invention or technical solution in the prior art
Specific implementation mode or attached drawing needed to be used in the description of the prior art are briefly described, it should be apparent that, it is described below
In attached drawing be that some embodiments of the utility model are not paying creativeness for those of ordinary skill in the art
Under the premise of labour, other drawings may also be obtained based on these drawings.
Fig. 1 is a kind of structure connection figure for rotor wing unmanned aerial vehicle auxiliary landing device that the utility model embodiment provides；
Fig. 2 is a kind of structural schematic diagram for rotor wing unmanned aerial vehicle auxiliary landing device that the utility model embodiment provides.
Icon：
The airplane parking areas 100- control terminal；The airplane parking areas 110- controller；120- magnetic induction sensors；130- magnetic locking devices；
131- electromagnet；132- pressure sensors；133- controls relay；134- third power supplys；200- unmanned aerial vehicle (UAV) controls end；210- without
Human-machine Control device；220- motors；230- roller bearings；240- ropes；250- magnetic patch；The first power supplys of 300-；400- second sources；500-
Position sensor.
Specific implementation mode
To keep the purpose, technical scheme and advantage of the utility model embodiment clearer, below in conjunction with attached drawing to this
The technical solution of utility model is clearly and completely described, it is clear that described embodiment is that the utility model part is real
Example is applied, instead of all the embodiments.Based on the embodiments of the present invention, those of ordinary skill in the art are not making
The every other embodiment obtained under the premise of creative work, shall fall within the protection scope of the present invention.
Currently, rotor wing unmanned aerial vehicle is based primarily upon artificial vision or nothing when automatic or manual operation is landed
Man-machine simple sensor balances to control, and under non-stable operating environment, the sight of people and single sensor hold very much
It is vulnerable to interference, unmanned gyroplane is easy to topple, and gently then blade is damaged, heavy then set to motor and the important instrument of carrying
It is standby to damage, it is based on this, a kind of rotor wing unmanned aerial vehicle auxiliary landing device that the utility model embodiment provides, it is ensured that nothing
The accuracy of man-machine landing place accelerates the sinking speed of unmanned plane, reduces the interference in unmanned plane descent, improves landing
Safety.
Referring to Fig. 1, a kind of structural schematic diagram for rotor wing unmanned aerial vehicle auxiliary landing device that the utility model embodiment provides.
The utility model embodiment provides a kind of rotor wing unmanned aerial vehicle auxiliary landing device, includes the airplane parking area control on airplane parking area
End 100 processed and the unmanned aerial vehicle (UAV) control end 200 inside unmanned plane.Airplane parking area control terminal and unmanned aerial vehicle (UAV) control end phase interworking
It closes, realizes the landing of unmanned plane.Airplane parking area control terminal 100 is connect with the first power supply 300, unmanned aerial vehicle (UAV) control end 200 and the second electricity
Source 400 connects, and is mounted on the bottom of unmanned plane, and control terminal passes through power supply power supply connected to it respectively.The device makes rotor
Unmanned plane reduces influence of the windage to aircraft when mobile platform lands, and realizes aircraft and is reliably landed in platform.
Specifically, airplane parking area control terminal 100 includes：Airplane parking area controller 110, magnetic induction sensor 120 and magnetic locking
Device 130, airplane parking area controller 110 are connected with magnetic induction sensor 120 and magnetic locking device 130 respectively.Airplane parking area control
Device processed is for realizing the data signal transmission between unmanned plane airplane parking area and unmanned plane, and magnetic induction sensor is for detecting electromagnetism letter
Number, magnetic locking device is used to limit the relative distance between airplane parking area and unmanned plane.
The falling signal that user terminal outside airplane parking area controller reception is sent, airplane parking area controller is according to falling signal
Start the ancillary equipment of landing, airplane parking area controller generates induction enabling signal according to the falling signal, and induction is started letter
It number is sent to magnetic induction sensor, magnetic induction sensor is started according to induction enabling signal, after magnetic induction sensor starts
Magnetic bodies in induction range is detected, when detect there is magnetic bodies after, magnetic induction sensor generate magnetic key operated lock
Tight signal.In the rotor wing unmanned aerial vehicle auxiliary landing device that the utility model embodiment provides, magnetic bodies is to be arranged in unmanned plane
The magnetic patch of bottom, when detect there is magnetic patch after, magnetic induction sensor generate magnetic locking signal.Magnetic induction sensor is by the magnetic
Power locking signal is sent to magnetic locking device by airplane parking area controller, and magnetic locking device is according to magnetic locking signal enabling
Locking to magnetic patch attracts magnetic patch in airplane parking area induction region, movement of the limitation magnetic patch relative to airplane parking area, magnetic locking
Device judges whether unmanned plane is successfully locked according to the pressure sensor being arranged in airplane parking area induction region, works as pressure sensing
When the numerical value that device detects reaches preset pressure value, defines unmanned plane and be locked, magnetic locking device is according to the lock of unmanned plane
Tight situation generates locking state signal.Specifically, when unmanned plane is locked, pressure sensor generates locking state signal.Magnetic
Power locking device sends locking state signal to the unmanned aerial vehicle (UAV) control device at unmanned aerial vehicle (UAV) control end by airplane parking area controller.
Further, in the rotor wing unmanned aerial vehicle auxiliary landing device that the utility model embodiment provides, magnetic locking device
130 include：Electromagnet 131, pressure sensor 132, control relay 133 and third power supply 134.Control relay respectively with electricity
Magnet, pressure sensor are connected with third power supply.Relay is controlled by third power supply power supply, control relay is according to shutdown
The magnetic locking signal enabling electromagnet locking that level ground controller is sent, controls relay conducting at this time, and electromagnet is connected into circuit
And with magnetism, attract the magnetic patch being connect with unmanned plane, when magnetic patch moves closer to simultaneously be locked in and stop finally due to magneticaction
When on the surface of machine level ground, when the numerical value that pressure sensor detects reaches preset pressure value, defines unmanned plane and be locked, pressure passes
Sensor generates locking state signal, and sends locking state signal to airplane parking area controller, and airplane parking area controller sends locking shape
State signal to unmanned aerial vehicle (UAV) control end unmanned aerial vehicle (UAV) control device.
Referring to Fig. 2, a kind of structural schematic diagram for rotor wing unmanned aerial vehicle auxiliary landing device that the utility model embodiment provides.
Specifically, unmanned aerial vehicle (UAV) control end 200 includes：Unmanned aerial vehicle (UAV) control device 210, motor 220, roller bearing 230, rope 240 and magnetic patch 250.
Unmanned aerial vehicle (UAV) control device, which is connected to the motor, to be connect, and motor is connected with roller bearing, and the outside of roller bearing is wound with rope, and one end of rope is fixed on
On roller bearing, the other end is fixed with magnetic patch.Unmanned aerial vehicle (UAV) control device is used to control start and stop and the signal of other equipment connected to it
The transmission of data, motor, roller bearing and rope realize the control of distance between magnetic patch and unmanned plane as transmission mechanism, to control
The distance between airplane parking area and unmanned plane, to realize the reliable landing of unmanned plane.When the technical solution avoids unmanned plane landing,
The gyroplane occurred due to controlling balance because of vision or simple sensor topples, and the landing difficulty of unmanned plane is reduced, to slow
The unmanned plane of the existing technology technical problem big in the platform landing difficulty of high-speed mobile is solved.
Unmanned aerial vehicle (UAV) control device receives the falling signal that external user terminal is sent, and unmanned aerial vehicle (UAV) control device is according to the falling signal
Electric motor starting signal is generated, realizes that magnetic patch is discharged to the direction far from fuselage, during magnetic patch constantly discharges, unmanned plane exists
Spiral above airplane parking area induction zone, and close to the region, with realize the realization of airplane parking area induction zone and magnetic patch carry out induction and
Locking, unmanned aerial vehicle (UAV) control device generate electric motor starting signal also according to locking state signal, realize the position where fuselage to magnetic patch
Close, during close, unmanned plane is in the accompanying flying state spiraled, and is in-flight drawn by rope.Motor according to
Corresponding electric motor starting signal drives roller bearing rotation, and while roller bearing rotates, the rope being secured to is realized release or received
Tightly, to realize the purpose for the length for adjusting rope release, and then the control of distance between magnetic patch and unmanned plane is realized.The technical side
Case realizes the steady safety of unmanned plane, fast and accurately lands, and while ensure that the accuracy of unmanned plane landing place, accelerates
The sinking speed of unmanned plane, reduces the interference in unmanned plane descent, improves the safety of landing.
Further, in the rotor wing unmanned aerial vehicle auxiliary landing device that the utility model embodiment provides, electric motor starting signal
Including rotating forward release signal and reversion tightening signal.Specifically, motor drives roller bearing to rotate forward according to release signal is rotated forward, roller bearing is just
When turning, increase the length of rope release, magnetic patch is discharged to the direction far from fuselage.Motor drives rolling also according to reversion tightening signal
Axis inverts, and when roller bearing inverts, reduces the length of rope release, the distance between unmanned plane and magnetic patch reduce.
Further, the rotor wing unmanned aerial vehicle auxiliary landing device that the utility model embodiment provides further includes and unmanned plane
The position sensor 500 that controller 210 is connected.Position sensor is used to detect the position of magnetic patch, when unmanned plane and magnetic patch it
Between distance when being decreased to preset distance value, define unmanned plane and landing be completed, position sensor is according to current magnetic patch
Position generates motor braking signal, and sends motor braking signal to motor by unmanned aerial vehicle (UAV) control device, and motor is according to motor system
Dynamic signal braking, to stop the tightening of rope, unmanned plane completes landing.
The rotor wing unmanned aerial vehicle auxiliary landing device that the utility model embodiment is provided, includes stopping on airplane parking area
Machine level ground control terminal and the unmanned aerial vehicle (UAV) control end inside unmanned plane.Airplane parking area control terminal and unmanned aerial vehicle (UAV) control end are separately connected
There are the first power supply and second source.Airplane parking area control terminal includes：Airplane parking area controller, magnetic induction sensor and magnetic locking dress
It sets.Airplane parking area controller is connected with magnetic induction sensor and magnetic locking device respectively.Airplane parking area controller receives landing letter
Number, and induction enabling signal is generated according to falling signal, magnetic induction sensor generates magnetic locking according to induction enabling signal to be believed
Number, magnetic locking device is locked according to magnetic locking signal enabling, generates locking state signal, and send out by airplane parking area controller
Send locking state signal.Unmanned aerial vehicle (UAV) control end includes：Unmanned aerial vehicle (UAV) control device, motor, roller bearing, rope and magnetic patch.Unmanned aerial vehicle (UAV) control
Device, which is connected to the motor, to be connect, and motor is connected with roller bearing, and the outside of roller bearing is wound with rope, and one end of rope is fixed on roller bearing, separately
One end is fixed with magnetic patch.Unmanned aerial vehicle (UAV) control device receives falling signal, and generates motor according to falling signal or locking state signal
Enabling signal, motor drive roller bearing to rotate according to electric motor starting signal, and adjust the length of rope release.The technical solution passes through
Airplane parking area control terminal and unmanned aerial vehicle (UAV) control end match in device, realize the steady safety of unmanned plane, fast and accurately land, protect
While having demonstrate,proved the accuracy of unmanned plane landing place, the sinking speed of unmanned plane is accelerated, reduces unmanned plane descent
In interference, improve the safety of landing, avoid because vision or simple sensor are come the gyroplane that occurs due to controlling balance
It topples, reduces the landing difficulty of unmanned plane, dropped in the platform of high-speed mobile to alleviate unmanned plane of the existing technology
The big technical problem of degree of meeting with misfortune.
In the description of the utility model embodiment unless specifically defined or limited otherwise, term " installation ", " phase
Even ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
Can also be electrical connection to be mechanical connection；It can be directly connected, can also indirectly connected through an intermediary, Ke Yishi
Connection inside two elements.For the ordinary skill in the art, above-mentioned term can be understood at this with concrete condition
Concrete meaning in utility model.
It is in the description of the present invention, it should be noted that term "center", "upper", "lower", "left", "right", " perpendicular
Directly ", the orientation or positional relationship of the instructions such as "horizontal", "inner", "outside" is to be based on the orientation or positional relationship shown in the drawings, and is only
The utility model and simplifying describes for ease of description, do not indicate or imply the indicated device or element must have it is specific
Orientation, with specific azimuth configuration and operation, therefore should not be understood as limiting the present invention.In addition, term " the
One ", " second ", " third " are used for description purposes only, and are not understood to indicate or imply relative importance.
Finally it should be noted that：Embodiment described above, only specific embodiment of the present utility model, to illustrate this
The technical solution of utility model, rather than its limitations, the scope of protection of the utility model is not limited thereto, although with reference to aforementioned
The utility model is described in detail in embodiment, it will be understood by those of ordinary skill in the art that：It is any to be familiar with this skill
The technical staff in art field within the technical scope disclosed by the utility model, still can be to the skill recorded in previous embodiment
Art scheme modify or can readily occur in variation or equivalent replacement of some of the technical features；And these modifications,
Variation is replaced, the spirit and model of the utility model embodiment technical solution that it does not separate the essence of the corresponding technical solution
It encloses, should be covered within the scope of the utility model.Therefore, the scope of protection of the utility model should be wanted with the right
Subject to the protection domain asked.
Claims (4)
1. a kind of rotor wing unmanned aerial vehicle auxiliary landing device, which is characterized in that include the airplane parking area control terminal on airplane parking area
With the unmanned aerial vehicle (UAV) control end inside unmanned plane；
The airplane parking area control terminal and unmanned aerial vehicle (UAV) control end are connected separately with the first power supply and second source；
The airplane parking area control terminal includes：Airplane parking area controller, magnetic induction sensor and magnetic locking device；
The airplane parking area controller is connected with the magnetic induction sensor and magnetic locking device respectively；
The airplane parking area controller receives falling signal, and generates induction enabling signal, the magnetic strength according to the falling signal
Inductive sensing device generates magnetic locking signal according to the induction enabling signal, and the magnetic locking device is according to the magnetic locking
Signal enabling is locked, and generates locking state signal, and send the locking state signal by the airplane parking area controller；
The unmanned aerial vehicle (UAV) control end includes：Unmanned aerial vehicle (UAV) control device, motor, roller bearing, rope and magnetic patch；
The unmanned aerial vehicle (UAV) control device is connected with the motor, and the motor is connected with the roller bearing, the outside of the roller bearing
It is wound with the rope, one end of the rope is fixed on the roller bearing, and the other end is fixed with the magnetic patch；
The unmanned aerial vehicle (UAV) control device receives falling signal, and generates electric motor starting according to the falling signal or locking state signal
Signal, the motor drive the roller bearing to rotate according to the electric motor starting signal, and adjust the length of the rope release.
2. the apparatus according to claim 1, which is characterized in that the magnetic locking device includes：Electromagnet, pressure sensing
Device, control relay and third power supply；
The control relay is connected with the electromagnet, pressure sensor and third power supply respectively；
The control relay is locked according to the magnetic locking signal enabling electromagnet, and the pressure sensor generates the lock
Tight status signal sends the locking state signal to the airplane parking area controller.
3. the apparatus according to claim 1, which is characterized in that the electric motor starting signal is including rotating forward release signal and instead
Turn tightening signal；
The motor drives the roller bearing to rotate forward according to the rotating forward release signal, and increases the length of the rope release；
The motor tightens signal according to the reversion and the roller bearing is driven to invert, and reduces the length of the rope release.
4. the apparatus according to claim 1, which is characterized in that further include the position being connected with the unmanned aerial vehicle (UAV) control device
Sensor；
The position sensor generates and sends motor braking signal according to the position of the magnetic patch；
The motor is braked according to the motor braking signal.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721669210.5U CN207712312U (en) | 2017-12-05 | 2017-12-05 | A kind of rotor wing unmanned aerial vehicle auxiliary landing device |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721669210.5U CN207712312U (en) | 2017-12-05 | 2017-12-05 | A kind of rotor wing unmanned aerial vehicle auxiliary landing device |
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| CN207712312U true CN207712312U (en) | 2018-08-10 |
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| CN201721669210.5U Active CN207712312U (en) | 2017-12-05 | 2017-12-05 | A kind of rotor wing unmanned aerial vehicle auxiliary landing device |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109305337A (en) * | 2018-09-30 | 2019-02-05 | 三汽车制造有限公司 | Unmanned plane, unmanned plane park platform and rising and dropping control method |
| CN109502041A (en) * | 2019-01-07 | 2019-03-22 | 吉林大学 | A kind of automatic landing-gear of vehicle-mounted rotor craft and control method |
| CN109760848A (en) * | 2019-02-27 | 2019-05-17 | 上海交通大学 | A kind of unmanned plane landing anti-skidding locking mechanism of unmanned boat |
| CN110745253A (en) * | 2019-10-31 | 2020-02-04 | 绍兴文理学院元培学院 | Accurate landing guiding device of unmanned aerial vehicle |
| CN111982580A (en) * | 2019-05-21 | 2020-11-24 | 中国石油天然气股份有限公司 | Unmanned aerial vehicle automatic oil extraction sampling system and method |
| CN112660405A (en) * | 2020-12-25 | 2021-04-16 | 上海大学 | Electromagnetic adsorption high-fault-tolerance unmanned aerial vehicle deployment and recovery system and unmanned aerial vehicle deployment and recovery method |
| CN115167522A (en) * | 2022-08-12 | 2022-10-11 | 深圳市人工智能与机器人研究院 | Landing system, landing method and storage medium for unmanned aerial vehicle |
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2017
- 2017-12-05 CN CN201721669210.5U patent/CN207712312U/en active Active
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109305337A (en) * | 2018-09-30 | 2019-02-05 | 三汽车制造有限公司 | Unmanned plane, unmanned plane park platform and rising and dropping control method |
| CN109502041A (en) * | 2019-01-07 | 2019-03-22 | 吉林大学 | A kind of automatic landing-gear of vehicle-mounted rotor craft and control method |
| CN109760848A (en) * | 2019-02-27 | 2019-05-17 | 上海交通大学 | A kind of unmanned plane landing anti-skidding locking mechanism of unmanned boat |
| CN109760848B (en) * | 2019-02-27 | 2021-01-22 | 上海交通大学 | Unmanned aerial vehicle descends unmanned ship and uses anti-skidding locking mechanical system |
| CN111982580A (en) * | 2019-05-21 | 2020-11-24 | 中国石油天然气股份有限公司 | Unmanned aerial vehicle automatic oil extraction sampling system and method |
| CN111982580B (en) * | 2019-05-21 | 2022-08-30 | 中国石油天然气股份有限公司 | Unmanned aerial vehicle automatic oil extraction sampling system and method |
| CN110745253A (en) * | 2019-10-31 | 2020-02-04 | 绍兴文理学院元培学院 | Accurate landing guiding device of unmanned aerial vehicle |
| CN112660405A (en) * | 2020-12-25 | 2021-04-16 | 上海大学 | Electromagnetic adsorption high-fault-tolerance unmanned aerial vehicle deployment and recovery system and unmanned aerial vehicle deployment and recovery method |
| CN115167522A (en) * | 2022-08-12 | 2022-10-11 | 深圳市人工智能与机器人研究院 | Landing system, landing method and storage medium for unmanned aerial vehicle |
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