CN109305336A - A kind of device and method that unmanned plane guidance is landed and fixed - Google Patents
A kind of device and method that unmanned plane guidance is landed and fixed Download PDFInfo
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- CN109305336A CN109305336A CN201811086235.1A CN201811086235A CN109305336A CN 109305336 A CN109305336 A CN 109305336A CN 201811086235 A CN201811086235 A CN 201811086235A CN 109305336 A CN109305336 A CN 109305336A
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- unmanned plane
- magnetic force
- landed
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- 230000003028 elevating effect Effects 0.000 claims description 10
- 239000007787 solid Substances 0.000 claims description 7
- 230000005540 biological transmission Effects 0.000 claims description 5
- 229910052742 iron Inorganic materials 0.000 claims description 5
- 229910052751 metal Inorganic materials 0.000 claims description 5
- 230000005294 ferromagnetic effect Effects 0.000 claims description 4
- 239000002184 metal Substances 0.000 claims description 4
- 238000009434 installation Methods 0.000 claims description 3
- 229920000742 Cotton Polymers 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 230000008859 change Effects 0.000 description 2
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- 241000208340 Araliaceae Species 0.000 description 1
- 235000005035 Panax pseudoginseng ssp. pseudoginseng Nutrition 0.000 description 1
- 235000003140 Panax quinquefolius Nutrition 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005288 electromagnetic effect Effects 0.000 description 1
- 230000005307 ferromagnetism Effects 0.000 description 1
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- 229910052759 nickel Inorganic materials 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
-
- 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
-
- 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
- B64F1/12—Anchoring
Abstract
The invention discloses the device and methods that a kind of guidance of unmanned plane is landed and fixed, and wherein device includes: the first guidance fixation member, is mounted on unmanned plane；Second guidance fixation member is mounted on wait place of landing, is attracted each other between the second guidance fixation member and the first guidance fixation member by magnetic field force；Magnetic force on off mechanism, for controlling the magnetic force on-off between the first guidance fixation member and the second guidance fixation member.The device of the invention and method guide the magnetic force on-off between fixation member and the second guidance fixation member by the action control first of magnetic force on off mechanism, specified region can not be precisely dropped to when solving unmanned plane in the prior art landing, problem troublesome in poeration when fixing and taking off again.
Description
Technical field
The present invention relates to unmanned plane landing and technique for fixing fields, guide and land in particular to a kind of unmanned plane
And fixed device and method.
Background technique
Existing unmanned plane can not precisely drop to specified region in landing；After landing, generally require artificial or mechanical
Intervene, unmanned plane could be made to reach specified range, to realize storage.
In addition, being required to disassembly horn when large-scale rotor wing unmanned aerial vehicle transport, foam cotton detent is generallyd use when fixed and is fixed,
It is placed individually into fixed detent cotton slot, needs again to load onto horn or blade in operation, it is troublesome in poeration, and be easy to cause
Interface fatigue damage.And under emergency scene, if vehicle roof needs to launch unmanned plane, such case dismounts unmanned plane horn
Then it can extremely expend the time.
Therefore, unmanned plane is able to guide there is an urgent need to develop one kind and drop to specified range, go to entangle without labor intensive again
Positive position, dismounting horn, while the fixed structure that unmanned plane can be made directly to take off rapidly, to meet showing for unmanned plane field
Real demand.
Summary of the invention
The main purpose of the present invention is to provide the device and methods that a kind of guidance of unmanned plane is landed and fixed, existing to solve
Specified region can not be precisely dropped to when having the unmanned plane landing in technology, problem troublesome in poeration when fixing and taking off again.
To achieve the goals above, according to an aspect of the invention, there is provided a kind of guidance of unmanned plane is landed and fixed
Device, comprising: first guidance fixation member, be mounted on unmanned plane；Second guidance fixation member, is mounted on wait place of landing,
It is attracted each other between second guidance fixation member and the first guidance fixation member by magnetic field force；Magnetic force on off mechanism, for controlling
Magnetic force on-off between the first guidance fixation member of system and the second guidance fixation member.
Further, the first guidance fixation member is the ferromagnetic metal component being mounted on unmanned plane, and the second guidance is solid
Determining component is the strong magnet for being mounted on place to be landed.
Further, the second guidance fixation member is permanent magnet.
Further, the first guidance fixation member is the iron pipe being fixedly mounted on the foot prop of unmanned plane.
Further, magnetic force on off mechanism includes: magnetoresistive component；Driving mechanism is connect with magnetoresistive component, for driving magnetic
Component movement is hindered, to control the magnetic force on-off between the first guidance fixation member and the second guidance fixation member.
Further, magnetoresistive component is the magnetic resistance being arranged between the first guidance fixation member and the second guidance fixation member
Piece, driving mechanism are motor, and magnetoresistive bit is mounted in the rotary shaft of motor.
Further, magnetoresistive component is the magnetic resistance being arranged between the first guidance fixation member and the second guidance fixation member
Piece, driving mechanism are cylinder or hydraulic cylinder, and magnetoresistive bit is mounted on the piston rod of cylinder or hydraulic cylinder.
Further, magnetic force on off mechanism includes: elevating mechanism, and elevating mechanism connect with the second guidance fixation member, uses
Fixation member is guided to rise or fall relative to the first guidance fixation member in driving second.
Further, at least two first guidance fixation members are installed, place corresponds to each the wait land on unmanned plane
One guidance fixation member is separately installed with one second guidance fixation member, each group first guidance fixation member and the second guidance
Fixation member is configured with magnetic force on off mechanism.
According to another aspect of the present invention, a kind of guidance of unmanned plane is provided to land and fixed method, on unmanned plane and
Place to be landed is equipped with above-mentioned device, method includes the following steps:
When unmanned plane is close to when place of landing needs to land, the movement of magnetic force on off mechanism, make the first guidance fixation member and
Magnetic force transmission is realized between second guidance fixation member, and unmanned plane is towed to place to be landed under the action of a magnetic force and is consolidated
It is fixed；
When unmanned plane needs to take off, the movement of magnetic force on off mechanism makes the first guidance fixation member and second guide fixation
Magnetic force between component disconnects, and unmanned plane is released and fixed.
It applies the technical scheme of the present invention, unmanned plane is made close to when place of landing needs to land by magnetic force on off mechanism
Magnetic force transmission is realized between first guidance fixation member and the second guidance fixation member, and unmanned plane is led under the action of a magnetic force
It leads to and specified to drop zone and is fixed；When unmanned plane needs to take off again, first is set to draw by magnetic force on off mechanism
The magnetic force led between fixation member and the second guidance fixation member disconnects, and unmanned plane can release fixation and take off.Pass through magnetic
The action control first of power on off mechanism guides the magnetic force on-off between fixation member and the second guidance fixation member, can be realized
The precision approach of unmanned plane, and unmanned plane is fixed and is not necessarily to dismount horn when taking off again, and the operation is more convenient.
Detailed description of the invention
The accompanying drawings constituting a part of this application is used to provide further understanding of the present invention, and of the invention shows
Examples and descriptions thereof are used to explain the present invention for meaning property, does not constitute improper limitations of the present invention.In the accompanying drawings:
Fig. 1 is structural schematic diagram of the device of an embodiment of the present invention when unmanned plane is in stationary state.
Fig. 2 is structural schematic diagram of the device of an embodiment of the present invention when unmanned plane is in takeoff condition.
Wherein, the above drawings include the following reference numerals:
10, the first guidance fixation member；20, the second guidance fixation member；30, magnetic force on off mechanism；31, magnetoresistive component；
32, driving mechanism；100, unmanned plane；110, foot prop.
Specific embodiment
To facilitate the understanding of the present invention, the present invention is made below in conjunction with Figure of description and preferred embodiment more complete
Face meticulously describes, but the protection scope of the present invention is not limited to the following specific embodiments.
Unless otherwise defined, all technical terms used hereinafter and the normally understood meaning of those skilled in the art
It is identical." first ", " second " used in present patent application specification and claims and similar word are simultaneously
Any sequence, quantity or importance are not indicated, and are intended merely to facilitate and corresponding components are distinguished.Equally, " one
It is a " or the similar word such as " one " do not indicate that quantity limits, but indicate that there are at least one.The classes such as " connection " or " connected "
As word be not limited to physics or mechanical connection, but may include electrical connection, either it is direct also
It is indirect."upper", "lower", "left", "right" etc. are only used for indicating relative positional relationship, when the absolute position for being described object changes
After change, then the relative positional relationship also correspondingly changes.
In order to precisely drop to specified region when solving unmanned plane in the prior art landing, fixes and take off again
When problem troublesome in poeration, land the present invention provides a kind of guidance of unmanned plane and fixed device and method.
Figures 1 and 2 show that unmanned plane guidance of the present invention is landed and a kind of embodiment of fixed device.Referring to Fig. 1 and
Fig. 2, unmanned plane guidance is landed and fixed device includes that the first guidance fixation member 10, second guides fixation member 20 and magnetic
Power on off mechanism 30.Wherein, the first guidance fixation member 10 is mounted on unmanned plane 100；Second guidance fixation member 20 is installed
Pass through magnetic field wait place of landing, and between the second guidance fixation member 20 and the first guidance fixation member 10 in unmanned plane 100
Power attracts each other；Magnetic force on off mechanism 30 is for controlling between the first guidance fixation member 10 and the second guidance fixation member 20
Magnetic force on-off.
The device for being landed and being fixed using above-mentioned unmanned plane guidance, unmanned plane 100 is close when place of landing needs to land,
Make to realize magnetic force transmission, nothing between the first guidance fixation member 10 and the second guidance fixation member 20 by magnetic force on off mechanism 30
Man-machine 100 are towed to specified to drop zone and are fixed under the action of a magnetic force；Unmanned plane 100 needs to rise again
When flying, keep the magnetic force between the first guidance fixation member 10 and the second guidance fixation member 20 disconnected by magnetic force on off mechanism 30
It opens, unmanned plane 100 can release fixation and take off.Fixation member is guided by the action control first of magnetic force on off mechanism 30
10 and second guidance fixation member 20 between magnetic force on-off, the precision approach of unmanned plane 100, and unmanned plane can be realized
100 are not necessarily to dismount horn when fixing and taking off again, and the operation is more convenient.
Specifically, in the present embodiment, the first guidance fixation member 10 is the ferromagnetic metal being mounted on unmanned plane 100
Component, the second guidance fixation member 20 is the strong magnet for being mounted on place to be landed.By installing ferromagnetism gold on unmanned plane 100
Metal elements (such as iron, cobalt, nickel or its alloy product), wait place's installation strong magnet that lands；Nobody is mounted on compared to by strong magnet
On machine 100, ferromagnetic metal component is mounted on to the mode at place to be landed, can avoid the magnetic field of strong magnet generation to unmanned plane
100 flight control system generates electromagnetic effect.
Further, in the present embodiment, the second guidance fixation member 20 preferably uses permanent magnet.Electromagnet is only logical
Attraction could be generated when electric；If will lead to electromagnet failure, the guidance of device and fixed effect will disappear because fortuitous event powers off
It loses.The present embodiment uses permanent magnet, avoids the case where generating failure because of power-off.In addition, in 100 transportational process of unmanned plane
In, it needs to fix unmanned plane 100 always by the second guidance fixation member 20, does not need to be constantly in energization using permanent magnet
State, and electromagnet needs is used to be always maintained at energization, it is in contrast, more energy saving and reliable using permanent magnet.
It is mutual by magnetic field force between the first guidance fixation member 10 and the second guidance fixation member 20 in order to preferably make
Attract, preferably guidance unmanned plane 100 drops to specified band drop zone, and unmanned plane 100 is carried out to preferably fixed, ginseng
See Fig. 1 and Fig. 2, the first guidance fixation member 10 is fixedly mounted on the foot prop 110 of unmanned plane 100.Specifically, by first
Guidance fixation member 10 is fixedly mounted on the bottom bar of foot prop 110, and guidance fixation member 10 can be such as used as using iron pipe,
Iron pipe fixation is set on the bottom bar of foot prop 110.In this way, the first guidance fixation member 10 and the second guidance can be shortened
The distance between fixation member 20 makes unobstructed, increase between the first guidance fixation member 10 and the second guidance fixation member 20
Magnetic field force between first guidance fixation member 10 and the second guidance fixation member 20, is more conducive to unmanned plane 100 accurately
It drops to wait place of landing, and unmanned plane 100 is fixedly secured.
Referring to Fig. 1 and Fig. 2, in order to further increase accuracy when unmanned plane 100 lands, and keep unmanned plane 100 fixed
It is stronger, at least two first guidance fixation members 10 are installed in the present embodiment, on unmanned plane 100, locate to correspond to wait land
One second guidance fixation member 20, each group first guidance fixation member are installed respectively in each first guidance fixation member 10
10 and second guide fixation member 20 to be configured with magnetic force on off mechanism 30.10 He of fixation member is guided by setting multiple groups first
Second guidance fixation member 20, the magnetic field force for making it attract each other is stronger, so that unmanned plane 100 is more accurate when landing, it is fixed
Ground is also stronger.
It is possible to further be respectively provided between each group first guidance fixation member 10 and the second guidance fixation member 20
One magnetic force on off mechanism 30 can also control multiple groups first using a magnetic force on off mechanism 30 simultaneously and guide fixation member 10
And second guidance fixation member 20 between magnetic field force on-off.When using a magnetic force on off mechanism 30, the structure of device can be made
More simplify, while can ensure that the synchronism of multiple groups magnetic field force on-off.The multiple groups first guide fixation member 10 and the second guidance
Fixation member 20 is preferably symmetrically mounted on unmanned plane 100, and 100 stress of unmanned plane can be made more balanced.
It should be noted that the magnetic force on off mechanism 30 in the application can take various forms, as long as in unmanned plane 100
Land and can make mutually to inhale between the first guidance fixation member 10 and the second guidance fixation member 20 by magnetic field force when fixed
Draw, the magnetic field between the first guidance fixation member 10 and the second guidance fixation member 20 can be disconnected when unmanned plane 100 takes off
Power is fixed to release.
Referring to Fig. 1 and Fig. 2, in the present embodiment, magnetic force on off mechanism 30 includes magnetoresistive component 31 and driving mechanism 32.Its
In, the setting of magnetoresistive component 31 is between the first guidance fixation member 10 and the second guidance fixation member 20；Driving mechanism 32 and magnetic
It hinders component 31 to connect, for driving magnetoresistive component 31 to move, with the first guidance fixation member 10 of control and the second guidance fixed part
Magnetic force on-off between part 20.When unmanned plane 100 lands and is fixed, magnetoresistive component 31 is set to be not at first by driving mechanism 32
It guides between fixation member 10 and the second guidance fixation member 20, so that the first guidance fixation member 10 and the second guidance fixed part
It is attracted each other between part 20 by magnetic field force；When unmanned plane 100 takes off again, it is in magnetoresistive component 31 by driving mechanism 32
Between first guidance fixation member 10 and the second guidance fixation member 20, the first guidance fixation member is blocked by magnetoresistive component 31
10 and second guidance fixation member 20 between magnetic field force, make unmanned plane 100 release fix.
Specifically, in the present embodiment, magnetoresistive component 31 is that setting is solid in the first guidance fixation member 10 and the second guidance
Determine the magnetoresistive bit between component 20, driving mechanism 32 is motor, which is mounted in the rotary shaft of motor.Pass through motor
Rotation drives magnetoresistive bit to rotate between the first guidance fixation member 10 and the second guidance fixation member 20.Further, the magnetic
The shape for hindering piece can be fan-shaped or rectangle, when motor-driven magnetic resistance piece is turned to far from the first guidance fixation member 10 and second
When guiding fixation member 20, the first guidance fixation member 10 and the second guidance fixation member 20 attract each other；Work as motor-driven magnetic
When resistance piece turns between the first guidance fixation member 10 and the second guidance fixation member 20, the first guidance fixation member 10
It interacts with the second guidance fixation member 20 without magnetic field force.
In the embodiment not shown of the application one, magnetoresistive component 31 is similarly setting in the first guidance fixation member 10 and the
Magnetoresistive bit between two guidance fixation members 20, and driving mechanism 32 is cylinder or hydraulic cylinder, magnetoresistive bit is mounted on the cylinder
Or on the piston rod of hydraulic cylinder.The first guidance fixation member 10 is realized by cylinder or Driven by Hydraulic Cylinder magnetoresistive bit transverse shifting
And second guidance fixation member 20 between the magnetic line of force through and off.In addition to cylinder or hydraulic cylinder, driving mechanism 32 be can also be
Other existing structures for driving magnetoresistive bit transverse shifting.
In the another embodiment not shown of the application, magnetic force on off mechanism 30 include elevating mechanism, the elevating mechanism it is defeated
Outlet is connect with the second guidance fixation member 20, for driving the second guidance fixation member 20 relative to the first guidance fixation member
10 rise or fall.Second guidance fixation member 20 is liftably mounted on by elevating mechanism wait place of landing, when unmanned plane 100
When needing to land and is fixed, is risen by elevating mechanism driving the second guidance fixation member 20, shorten the first guidance fixation member
10 and second guide the distance between fixation member 20, increase its magnetic field force to attract each other；When unmanned plane 100 needs to rise again
When flying, is declined by elevating mechanism driving the second guidance fixation member 20, keep the first guidance fixation member 10 and the second guidance solid
Determine the increase of the distance between component 20, the magnetic field force for making it attract each other weakens significantly even to be disconnected, and releases unmanned plane 100 solid
It is fixed.The elevating mechanism can be the existing driving structure such as cylinder, hydraulic cylinder, linear motor.
Above-mentioned unmanned plane guidance is landed and the operation principle and using method of fixed device is as follows:
When unmanned plane 100 is close to when place of landing needs to land, control terminal (is mounted on place to be landed or unmanned plane 100)
It provides signal control magnetic force on off mechanism 30 to act, make real between the first guidance fixation member 10 and the second guidance fixation member 20
Existing magnetic force transmission (being attracted each other by magnetic field force), unmanned plane 100 are drop to by traction wait place of landing under the action of a magnetic force,
And it is fixed；
When unmanned plane 100 needs to take off, control terminal provides signal control magnetic force on off mechanism 30 and acts, and makes the first guidance
Magnetic force between fixation member 10 and the second guidance fixation member 20 disconnects, and unmanned plane 100 is released and fixed, and starts unmanned plane
100 can take off.
It can be seen from the above description that the above embodiments of the present invention realized the following chievements: of the invention
Scheme is logical by the magnetic force between first guidance fixation member 10 of the control of magnetic force on off mechanism 30 and the second guidance fixation member 20
It is disconnected, precision approach and the fixation of unmanned plane 100 can be realized, and unmanned plane 100 is fixed, transport and when taking off again without tearing open
Installation arm or blade operate quite convenient.Especially for the fixation and transport of relatively large gyroplane, using dress of the invention
Operation can effectively be simplified by setting, and unmanned plane 100 is allow directly to take off rapidly.
The foregoing is only a preferred embodiment of the present invention, is not intended to restrict the invention, for the skill of this field
For art personnel, the invention may be variously modified and varied.All within the spirits and principles of the present invention, made any to repair
Change, equivalent replacement, improvement etc., should all be included in the protection scope of the present invention.
Claims (10)
1. a kind of unmanned plane guidance is landed and fixed device characterized by comprising
First guidance fixation member (10), is mounted on unmanned plane (100)；
Second guidance fixation member (20) is mounted on wait place of landing, and second guidance fixation member (20) is drawn with described first
It leads and is attracted each other between fixation member (10) by magnetic field force；
Magnetic force on off mechanism (30), for controlling first guidance fixation member (10) and the second guidance fixation member
(20) the magnetic force on-off between.
2. unmanned plane guidance according to claim 1 is landed and fixed device, which is characterized in that first guidance is solid
Determining component (10) is the ferromagnetic metal component being mounted on the unmanned plane (100), second guidance fixation member (20)
For the strong magnet for being mounted on the place to be landed.
3. unmanned plane guidance according to claim 2 is landed and fixed device, which is characterized in that second guidance is solid
Determining component (20) is permanent magnet.
4. unmanned plane guidance according to claim 2 is landed and fixed device, which is characterized in that first guidance is solid
Determining component (10) is the iron pipe being fixedly mounted on the foot prop (110) of the unmanned plane (100).
5. unmanned plane guidance according to claim 1 is landed and fixed device, which is characterized in that the magnetic force on-off machine
Structure (30) includes:
Magnetoresistive component (31)；
Driving mechanism (32) is connect with the magnetoresistive component (31), for driving the magnetoresistive component (31) to move, to control
State the magnetic force on-off between the first guidance fixation member (10) and second guidance fixation member (20).
6. unmanned plane guidance according to claim 5 is landed and fixed device, which is characterized in that the magnetoresistive component
(31) magnetoresistive bit between fixation member (20), institute are guided in first guidance fixation member (10) and described second for setting
Stating driving mechanism (32) is motor, and the magnetoresistive bit is mounted in the rotary shaft of the motor.
7. unmanned plane guidance according to claim 5 is landed and fixed device, which is characterized in that the magnetoresistive component
(31) magnetoresistive bit between fixation member (20), institute are guided in first guidance fixation member (10) and described second for setting
Stating driving mechanism (32) is cylinder or hydraulic cylinder, and the magnetoresistive bit is mounted on the piston rod of the cylinder or hydraulic cylinder.
8. unmanned plane guidance according to claim 1 is landed and fixed device, which is characterized in that the magnetic force on-off machine
Structure (30) includes:
Elevating mechanism, the elevating mechanism are connect with second guidance fixation member (20), for driving second guidance
Fixation member (20) rises or falls relative to first guidance fixation member (10).
9. unmanned plane guidance according to claim 1 is landed and fixed device, which is characterized in that the unmanned plane
(100) at least two first guidance fixation member (10) are installed on, it is described to correspond to each described first wait place of landing
Guidance fixation member (10) is separately installed with second guidance fixation member (20), and the first guidance described in each group is fixed
Component (10) and second guidance fixation member (20) are configured with the magnetic force on off mechanism (30).
10. a kind of unmanned plane guidance is landed and fixed method, just like right on the unmanned plane (100) and wait place's installation of landing
It is required that device described in any one of 1-9, the described method comprises the following steps:
When the unmanned plane (100) are close described when place of landing needs to land, magnetic force on off mechanism (30) movement makes institute
It states and realizes magnetic force transmission, the unmanned plane between the first guidance fixation member (10) and second guidance fixation member (20)
(100) place to be landed is towed under the action of a magnetic force to be fixed；
When the unmanned plane (100) needs to take off, magnetic force on off mechanism (30) movement makes the first guidance fixed part
Magnetic force between part (10) and second guidance fixation member (20) disconnects, and the unmanned plane (100) releases fixation.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811086235.1A CN109305336A (en) | 2018-09-18 | 2018-09-18 | A kind of device and method that unmanned plane guidance is landed and fixed |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811086235.1A CN109305336A (en) | 2018-09-18 | 2018-09-18 | A kind of device and method that unmanned plane guidance is landed and fixed |
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