CN110104196A - A kind of the unmanned plane arresting gear and unmanned plane closing method of energy automatic shutter - Google Patents
A kind of the unmanned plane arresting gear and unmanned plane closing method of energy automatic shutter Download PDFInfo
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- CN110104196A CN110104196A CN201910506746.2A CN201910506746A CN110104196A CN 110104196 A CN110104196 A CN 110104196A CN 201910506746 A CN201910506746 A CN 201910506746A CN 110104196 A CN110104196 A CN 110104196A
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- unmanned plane
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- parking area
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- 230000008569 process Effects 0.000 claims abstract description 6
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- 238000010586 diagram Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 241000469816 Varus Species 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
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- 208000015181 infectious disease Diseases 0.000 description 1
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Classifications
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- 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
- B64F1/005—Protective coverings for aircraft not in use
-
- 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
- B64F1/007—Helicopter portable landing pads
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0011—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Power-Operated Mechanisms For Wings (AREA)
Abstract
The invention discloses the unmanned plane arresting gears and unmanned plane closing method of a kind of energy automatic shutter, including shutting down room, shut down the bottom plate that room includes square, the cover board that the vertical side plate on four side of bottom plate is set and is hingedly arranged at the top of vertical side plate, driving cover board rotation is provided at the top of vertical side plate opens ejection device, it shuts down room bottom and is provided with airplane parking area, the lower end of airplane parking area is provided with the lifting device that driving airplane parking area rises, shut down the shutdown positioning device that the stopping process offer location information of promising unmanned plane is set on room and unmanned plane, shutting down positioning device includes the shutdown positioned reflector lamp that unmanned plane edge is arranged in, the light receiver plate of airplane parking area upper surface and cover board lower surface is set, and the infrared remote sensor shut down within doors is set, the shutdown area of unmanned plane can be expanded, detect the position of unmanned plane, tilt angle and Flight orientation, reduces the shutdown difficulty of unmanned plane, and stability when enhancing unmanned plane lands guarantees the stop safe of unmanned plane.
Description
Technical field
The invention belongs to air vehicle technique field more particularly to it is a kind of can automatic shutter unmanned plane arresting gear and nobody
Machine closing method.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself
The not manned aircraft of presetting apparatus manipulation, or fully or intermittently automatically operated by car-mounted computer.With someone
It drives an airplane and compares, unmanned plane is often more suitable for the task of those too " slow-witted, dirty or dangerous ".Unmanned plane presses 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
Unmanned plane has really just needed；It taking photo by plane at present, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observing wild move
The application in object, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, greatly
The big purposes for having expanded unmanned plane itself, developed country also in actively extension industrial application and develop unmanned air vehicle technique.
In the prior art, unmanned plane usually drops out shutdown room in landing, needs that unmanned plane is put into shutdown within doors manually,
And the touch down attitude and landing angle of unmanned plane are unable to accurately control, and are needed people to manually adjust the angle of unmanned plane, are made nothing
Man-machine posture can be convenient for taking off again.
Summary of the invention
The purpose of the present invention is to provide the unmanned plane arresting gears and unmanned plane closing method of a kind of energy automatic shutter, can
Area is shut down to expand, reduces and shuts down difficulty, guarantees stop safe, and control the touch down attitude of unmanned plane, convenient for unmanned plane
It takes off again, to need to manually pick up caused by solving and usually drop out in landing due to unmanned plane in the prior art and shut down room
Unmanned plane, and need people to manually adjust nobody caused by being unable to accurately control due to unmanned plane touch down attitude with landing angle
The problem of angle of machine.
To achieve the goals above, embodiments of the present invention provide the following technical solutions:
It is a kind of can automatic shutter unmanned plane arresting gear, including shut down room, it is described shut down room include square bottom plate,
The cover board that the vertical side plate on four side of bottom plate is set and is hingedly arranged at the top of vertical side plate, the vertical side plate top setting
Have driving cover board rotation opens ejection device, and the shutdown room bottom is provided with airplane parking area, and the lower end of the airplane parking area is provided with drive
The lifting device that dynamic airplane parking area rises；
The shutdown positioning for shutting down the stopping process offer location information that promising unmanned plane is arranged on room and unmanned plane fills
It sets, the shutdown positioning device includes the shutdown positioned reflector lamp that the unmanned plane edge is arranged in, table is arranged on airplane parking area
The light receiver plate of face and cover board lower surface and the infrared remote sensor shut down within doors is set.
As a preferred solution of the present invention, the cover board is in isosceles right triangle shape, and top cover described in four
It is combined into square identical with bottom plate when closure, the shape and size of the airplane parking area and bottom plate are all the same.
As a preferred solution of the present invention, the ejection device of opening includes rotation axis, and the cover board is connected with rotation axis,
And the cover board being arranged radially along rotation axis.
As a preferred solution of the present invention, the upper end-face edge of the cover board is provided with vertical angle limit plate.
As a preferred solution of the present invention, the top both ends of the vertical side plate are provided with rotating steadying bar, and described turn
The both ends of moving axis are threaded through on rotating steadying bar, and top motor is provided with out on the rotating steadying bar described in one of them, described to open top electricity
Machine is connected with rotation axis.
As a preferred solution of the present invention, straight down, the shutdown positioned reflector lamp has the shutdown positioned reflector lamp
Several, several shutdown positioned reflector lamps sketch the contours of the edge shape of unmanned plane.
As a preferred solution of the present invention, the lifting device includes several lifting cylinders, the lifting cylinder
Output end is connected straight up and with the bottom of airplane parking area.
The present invention also provides a kind of unmanned plane closing methods, include the following steps:
S100, unmanned plane, which are moved to, shuts down near room, adjusts unmanned plane during flying posture；
S200, positioning light is issued, unmanned plane position and angle is determined according to positioning light；
S300, according to unmanned plane position and angle, adjust position and the angle of unmanned plane, unmanned plane made to be moved to shutdown room
Surface, then slowly land into shutdown within doors.
As a preferred solution of the present invention, the specific steps of above-mentioned S100 are as follows:
S101, unmanned plane are mobile to room is shut down, and incude unmanned plane by sensoring and shut down at a distance from room；
S102, after reaching distance of reaction, the flying speed of unmanned plane is reduced, prepared for the landing of unmanned plane；
S103, the state of flight for adjusting unmanned plane, are allowed to be maintained at horizontality, do standard for the subsequent positioning of unmanned plane
It is standby.
Embodiments of the present invention have the advantages that
(1) present invention is by being arranged liftable airplane parking area and four isosceles right triangle shapes that can turn down 180 degree
Cover board, when four cover board fold inward to levels, cover board will shut down the top closure in room, realize shut down room and it is extraneous every
Absolutely, avoid unmanned plane from contacting with external items, and when cover board is turned-out be folded to level when, four cover boards combine the shutdown risen
Level ground may make up a square shutdown platform, and the area of the platform is two times of airplane parking area, to expand stopping for unmanned plane
Machine side product, reduces the shutdown difficulty of unmanned plane, ensure that the stop safe of unmanned plane；
(2) present invention can provide positioning action by setting by shutdown positioning device for the stopping process of unmanned plane,
It detects the position of unmanned plane, be in fashion posture, tilt angle and flight orientation, so that unmanned plane be made to be adjusted to horizontal before landing
State, stability when enhancing unmanned plane lands, enables unmanned plane accurately to fall in shutdown within doors.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below
There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this
Some embodiments of invention without any creative labor, may be used also for those of ordinary skill in the art
To obtain other attached drawings according to these attached drawings.
Structure depicted in this specification, ratio, size etc., only to cooperate the revealed content of specification, for
Those skilled in the art understands and reads, and is not intended to limit the invention enforceable qualifications, therefore does not have technical
Essential meaning, the modification of any structure, the change of proportionate relationship or the adjustment of size are not influencing the function of the invention that can be generated
Under effect and the purpose that can reach, should all still it fall in the range of disclosed technology contents obtain and can cover.
Fig. 1 is the overall structure diagram in embodiment of the present invention；
Fig. 2 is the overlooking structure diagram in embodiment of the present invention；
Fig. 3 is the structural schematic diagram that ejection device is opened in embodiment of the present invention.
In figure:
1- shuts down room；2- opens ejection device；The airplane parking area 3-；4- lifting device；5- shuts down positioning device；
101- bottom plate；The vertical side plate of 102-；103- cover board；
201- rotation axis；202- angle limit plate；203- rotating steadying bar；204- opens top motor；
501- shuts down positioned reflector lamp；502- light receiver plate；503- infrared remote sensor.
Specific embodiment
In order to make the invention's purpose, features and advantages of the invention more obvious and easy to understand, below in conjunction with the present invention
Attached drawing in embodiment, technical scheme in the embodiment of the invention is clearly and completely described, it is clear that disclosed below
Embodiment be only a part of the embodiment of the present invention, and not all embodiment.Based on the embodiments of the present invention, this field
Those of ordinary skill's all other embodiment obtained without making creative work, belongs to protection of the present invention
Range.
As shown in Figure 1 to Figure 3, the present invention provides a kind of unmanned plane arresting gears of energy automatic shutter, including shut down room
1, the room 1 of shutting down includes that square bottom plate 101, the vertical side plate 102 that 101 4 side of bottom plate is arranged in and hinged setting exist
The cover board 103 at vertical 102 top of side plate, be provided with that driving cover board 103 rotates at the top of the vertical side plate 102 opens ejection device
2,1 bottom of shutdown room is provided with airplane parking area 3, and the lower end of the airplane parking area 3 is provided with the lifting dress risen driving airplane parking area 3
Set 4.
In the present invention, the cover board 103 be in isosceles right triangle shape, and top cover 103 described in four be closed when group
Square identical with bottom plate 101 is synthesized, the shape and size of the airplane parking area 3 and bottom plate 101 are all the same.When unmanned plane needs
When shutdown, opens ejection device 2 and cover board 103 is driven to flip up to horizontality, then lifting device 4 drives and moves on airplane parking area 3
It is flushed with cover board 103, airplane parking area 3 is connected with four cover boards 103 at this time, constitutes a complete square-shaped planar, can be with
For carrying unmanned plane.
In the above description, the plane formed when four cover boards 103 are closed is identical as the area of airplane parking area 3, so covering
After plate 103 is opened, airplane parking area 3 rises, the area of shutting down of unmanned plane is 2 times of airplane parking area 3, expands the shutdown face of unmanned plane
Product, reduces the shutdown difficulty of unmanned plane.
As shown in figures 1 and 3, in the present invention, the ejection device 2 of opening includes rotation axis 201, the cover board 103 with turn
Moving axis 201 is connected, and being arranged radially along rotation axis 201 of the cover board 103, the edge of the cover board 103 are vertically arranged with angle
Limit plate 202 is spent, the top both ends of the vertical side plate 102 are provided with rotating steadying bar 203, and the both ends of the rotation axis 201 are worn
It is located on rotating steadying bar 203, top motor 204 is provided with out on the rotating steadying bar 203 described in one of them, it is described to open top motor
204 are connected with rotation axis 201.
In the present invention, since cover board 103 is isosceles triangle, when cover board 103 is turned-out is folded to level, it is arranged at it
Angle limit plate 202 on side downwards, and is bonded with the outer wall of vertical side plate 102, continue cover board 103 can not downwards
Bending, is maintained at horizontality, and have certain support force, is parked on cover board 103 convenient for unmanned plane；And when cover board 103 to
When varus is folded to level, the angle limit plate 202 being arranged on two right-angle sides is vertical upward, with adjacent 103 right-angle side of cover board
On angle limit plate 202 be bonded, can equally make cover board 103 that can not continue to bend downward, be maintained at horizontality, prevent nobody
Cover board 103 falls into shutdown within doors when machine rests on shutdown within doors, so that unmanned plane be avoided to be destroyed.
As shown in Figure 1, in the present invention, the lifting device 4 includes several lifting cylinders, the output of the lifting cylinder
End is connected straight up and with the bottom of airplane parking area 3, and stretching and the retraction of lifting cylinder output end can control the liter of airplane parking area 3
It rises and lands.
Meanwhile landing as shown in Figure 1, promising unmanned plane is arranged in the present invention, on the shutdown room 1 and unmanned plane and shuts down
The shutdown positioning device 5 of location information is provided, the positioning device 5 of shutting down includes that the shutdown of the unmanned plane edge is arranged in
Positioned reflector lamp 501, the light receiver plate 502 that 103 lower surface of 3 upper surface of airplane parking area and cover board is arranged in and setting are being shut down
Infrared remote sensor 503 in room 1, straight down, the shutdown positioned reflector lamp 501 has several to the shutdown positioned reflector lamp 501,
Several shutdowns positioned reflector lamps 501 sketch the contours of the edge shape of unmanned plane, shutdown positioning device 5 further include for receiving,
The control chip of processing and transmission information, the chip can use AT89C51 single-chip microcontroller common on the market, control chip and light
Line receiver board 502 is connected.
It when unmanned plane needs to shut down, is moved to and is shut down near room 1 in unmanned plane, nothing is incuded by infrared remote sensor 503
It is man-machine after reaching distance of reaction, to reduce the flying speed of unmanned plane at a distance from shutdown room 1, it is that the landing of unmanned plane is valid
It is standby, while the state of flight of unmanned plane is adjusted, it is allowed to be maintained at horizontality, prepare for the subsequent positioning of unmanned plane, then
Positioned reflector lamp 501 is shut down in starting, is allowed to emit beam, then be received by light receiver plate 502.The shutdown positioned reflector lamp 501
There are several, several shutdown positioned reflector lamps 501 sketch the contours of the edge shape of unmanned plane, due to shutting down positioned reflector lamp 501
There are multiple, and these shut down the edge that positioned reflector lamps 501 are distributed in unmanned plane, will shut down the density setting of positioned reflector lamp 501
In the appropriate range, so that shutting down the flight that the light that positioned reflector lamp 501 projects can confirm the position of unmanned plane by detection
Posture, heading and tilt angle.It is radiated on light receiver plate 502 shutting down light front emitted by positioned reflector lamp 501
When, that is, indicate that unmanned plane is located at the surface (because unmanned plane is in horizontality, light is vertical at this time) of light receiver plate 502,
In can depression area, then control unmanned plane landing.
The present invention also provides a kind of unmanned plane closing method, comprising steps of S100, unmanned plane are moved to, to shut down room attached
Closely, incude unmanned plane by sensoring and shut down at a distance from room, after reaching distance of reaction, reduce the flight speed of unmanned plane
Degree prepares for the landing of unmanned plane, while adjusting the state of flight of unmanned plane, is allowed to be maintained at horizontality, is unmanned plane
Subsequent positioning prepare；
S200, positioning light is issued, unmanned plane position and angle is determined according to positioning light；
S300, according to unmanned plane position and angle, adjust position and the angle of unmanned plane, unmanned plane made to be moved to shutdown room
Surface, then slowly land into shutdown within doors.
By above-mentioned unmanned plane closing method, the present invention can guarantee that unmanned plane can be adjusted to horizontal before landing
State enables unmanned plane accurately to fall in shutdown within doors to enhance stability when unmanned plane landing.
The above, the above embodiments are merely illustrative of the technical solutions of the present invention, rather than its limitations；Although referring to before
Stating embodiment, invention is explained in detail, those skilled in the art should understand that: it still can be to preceding
Technical solution documented by each embodiment is stated to modify or equivalent replacement of some of the technical features；And these
It modifies or replaces, the spirit and scope for technical solution of various embodiments of the present invention that it does not separate the essence of the corresponding technical solution.
Claims (9)
1. a kind of unmanned plane arresting gear of energy automatic shutter, which is characterized in that including shutting down room (1), shutdown room (1) packet
It includes the bottom plate (101) of square, be arranged in the vertical side plate (102) on (101) four side of bottom plate and hinged setting in vertical side plate
(102) cover board (103) at the top of, driving cover board (103) rotation is provided at the top of the vertical side plate (102) opens ejection device
(2), shutdown room (1) bottom is provided with airplane parking area (3), and the lower end of the airplane parking area (3) is provided with driving airplane parking area (3) and rises
The lifting device (4) risen；
It is described to shut down the shutdown positioning device that the stopping process offer location information of promising unmanned plane is set on room (1) and unmanned plane
(5), shutdown positioning device (5) includes the shutdown positioned reflector lamp (501) that the unmanned plane edge is arranged in, is arranged and is stopping
The light receiver plate (502) and setting of machine level ground (3) upper surface and cover board (103) lower surface are infrared distant in shutdown room (1)
Sensor (503).
2. a kind of unmanned plane arresting gear of energy automatic shutter according to claim 1, which is characterized in that the cover board
(103) it is in isosceles right triangle shape, and is combined into when the closure of top cover (103) described in four identical just with bottom plate (101)
Rectangular, the airplane parking area (3) and the shape and size of bottom plate (101) are all the same.
3. a kind of unmanned plane arresting gear of energy automatic shutter according to claim 1, which is characterized in that described to open top dress
Setting (2) includes rotation axis (201), and the cover board (103) is connected with rotation axis (201), and the cover board (103) is along rotation axis
(201) be arranged radially.
4. a kind of unmanned plane arresting gear of energy automatic shutter according to claim 3, which is characterized in that the cover board
(103) upper end-face edge is provided with vertical angle limit plate (202).
5. a kind of unmanned plane arresting gear of energy automatic shutter according to claim 4, which is characterized in that described to open top dress
Setting (2) further includes rotating steadying bar (203) of the setting at the top both ends of vertical side plate (102), the both ends of the rotation axis (201)
It is threaded through on rotating steadying bar (203), top motor (204) is provided with out on the rotating steadying bar (203) described in one of them, it is described to open
Top motor (204) is connected with rotation axis (201).
6. a kind of unmanned plane arresting gear of energy automatic shutter according to claim 1, which is characterized in that described shut down is determined
Straight down, the shutdown positioned reflector lamp (501) has several to position shot-light (501), several shutdown positioned reflector lamps (501)
Sketch the contours of the edge shape of unmanned plane.
7. a kind of unmanned plane arresting gear of energy automatic shutter according to claim 1, which is characterized in that the lifting dress
Setting (4) includes several lifting cylinders, and the output end of the lifting cylinder is connected straight up and with the bottom of airplane parking area (3).
8. a kind of unmanned plane closing method, which comprises the steps of:
S100, unmanned plane, which are moved to, shuts down near room, adjusts unmanned plane during flying posture；
S200, positioning light is issued, unmanned plane position and angle is determined according to positioning light；
S300, according to unmanned plane position and angle, adjust position and the angle of unmanned plane, make unmanned plane be moved to shut down room just
Then top is slowly landed into shutdown within doors.
9. a kind of unmanned plane closing method according to claim 8, which is characterized in that the detailed process of the step S100
Are as follows:
S101, unmanned plane are mobile to room is shut down, and incude unmanned plane by sensoring and shut down at a distance from room；
S102, after reaching distance of reaction, the flying speed of unmanned plane is reduced, prepared for the landing of unmanned plane；
S103, the state of flight for adjusting unmanned plane, are allowed to be maintained at horizontality, prepare for the subsequent positioning of unmanned plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910506746.2A CN110104196A (en) | 2019-06-12 | 2019-06-12 | A kind of the unmanned plane arresting gear and unmanned plane closing method of energy automatic shutter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910506746.2A CN110104196A (en) | 2019-06-12 | 2019-06-12 | A kind of the unmanned plane arresting gear and unmanned plane closing method of energy automatic shutter |
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| Publication Number | Publication Date |
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| CN110104196A true CN110104196A (en) | 2019-08-09 |
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ID=67494774
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|---|---|---|---|
| CN201910506746.2A Pending CN110104196A (en) | 2019-06-12 | 2019-06-12 | A kind of the unmanned plane arresting gear and unmanned plane closing method of energy automatic shutter |
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| CN110435840A (en) * | 2019-08-16 | 2019-11-12 | 蚌埠市建金智能科技有限公司 | A kind of deck of boat with unmanned plane stop device |
| CN110844099A (en) * | 2019-10-21 | 2020-02-28 | 燕山大学 | Carrier-based stable platform with liftable and separable table top |
| CN111627062A (en) * | 2020-06-08 | 2020-09-04 | 星逻人工智能技术(上海)有限公司 | Aircraft shutdown state control method, device and device using method |
| CN115209090A (en) * | 2021-04-08 | 2022-10-18 | 北京高特通技术有限公司 | Wisdom city monitored control system |
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| CN111627062B (en) * | 2020-06-08 | 2021-02-05 | 星逻人工智能技术(上海)有限公司 | Aircraft shutdown state control method, device and device using method |
| CN115209090A (en) * | 2021-04-08 | 2022-10-18 | 北京高特通技术有限公司 | Wisdom city monitored control system |
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Application publication date: 20190809 |