CN110109507A - A kind of unmanned plane manipulation pedal - Google Patents
A kind of unmanned plane manipulation pedal Download PDFInfo
- Publication number
- CN110109507A CN110109507A CN201910461831.1A CN201910461831A CN110109507A CN 110109507 A CN110109507 A CN 110109507A CN 201910461831 A CN201910461831 A CN 201910461831A CN 110109507 A CN110109507 A CN 110109507A
- Authority
- CN
- China
- Prior art keywords
- pedal
- fixed
- unmanned plane
- rotor plate
- gear
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000006073 displacement reaction Methods 0.000 claims abstract description 31
- 230000006698 induction Effects 0.000 claims abstract description 15
- 238000013016 damping Methods 0.000 claims description 14
- 238000003780 insertion Methods 0.000 claims description 3
- 230000037431 insertion Effects 0.000 claims description 3
- 230000005540 biological transmission Effects 0.000 claims 1
- 201000009482 yaws Diseases 0.000 abstract description 2
- 238000013461 design Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 230000007812 deficiency Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000004088 simulation Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
- G05G1/00—Controlling members, e.g. knobs or handles; Assemblies or arrangements thereof; Indicating position of controlling members
- G05G1/30—Controlling members actuated by foot
- G05G1/34—Double foot controls, e.g. for instruction vehicles
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Mechanical Control Devices (AREA)
Abstract
The invention discloses a kind of unmanned planes to manipulate pedal, it includes the rotor plate of " H " shape, strip groove there are two being opened up on rotor plate, pedal base is provided in two strip grooves, it is provided with pedal on pedal base, fixed gear is provided in strip groove, and fixed gear extends into pedal base, induction gear is provided in pedal base, and induction gear is mounted on pedal base by the first angular displacement sensor；Pedal base is hinged on fixed gear, and induction gear is engaged with fixed gear；Fixed plate is connected with by rotation axis below rotor plate, the second angular displacement sensor detects rotational angle.This programme is manipulated applied to unmanned plane, and staff yaws unmanned plane, turns to and tilt etc. and operates by both feet.
Description
Technical field
The present invention relates to air vehicle technique fields, and in particular to a kind of unmanned plane manipulation pedal.
Background technique
It to the manipulation of unmanned plane is completed in flight monitoring seat, Mission Monitor seat in the prior art, by operating
Platform fitted underneath pedal；Operator steps on pedal by foot, realizes the control to unmanned plane；In unmanned aerial vehicle ground control system,
Control device is the important hardware for influencing unmanned plane during flying safety.Pedal belongs to a significant element in control device, mainly
It is responsible for the brake and Nose Wheel Steering control in unmanned aerial vehicle stage, and the yaw control in aerial stage, pedal are grasped by unmanned plane
Work person uses left and right foot control system.For crew station design personnel, pedal is required to meet the brake of unmanned plane, turning and boat
To the functional requirement of control, from flight operation person for, pedal needs reasonable dynamics, 18 length of suitable pedal and suitable
Installation site.Design about unmanned plane pedal is carrying out always in unmanned plane Project R&D, as certain A type unmanned plane pedal is adopted
It is partly to step on formula simulation pedal, certain B unmanned plane pedal using stepping on digital pedal entirely.It is general with unmanned aerial vehicle station
Change, pedal above is no longer satisfied different pilots to the operational requirements of different model unmanned plane.It is general due to pedal
Change the significant element that there are many factor in need of consideration, it is manipulated as influence unmanned plane, there is very big researching value.
Summary of the invention
For the above-mentioned deficiency of the prior art, the present invention provides a kind of better reduction, unmanned planes with high accuracy to manipulate
Pedal.
To achieve the above object of the invention, the technical scheme adopted by the invention is as follows:
A kind of unmanned plane manipulation pedal is provided comprising the rotor plate of " H " shape is opened up there are two strip groove on rotor plate,
It is provided with pedal base in two strip grooves, pedal is provided on pedal base, fixed gear, and fixed tooth are provided in strip groove
Wheel extends into pedal base, induction gear is provided in pedal base, and induction gear is mounted on by the first angular displacement sensor
On pedal base；Pedal base is hinged on fixed gear, and induction gear is engaged with fixed gear；
Fixed plate is connected with by rotation axis below rotor plate, and rotation axis is fixed in fixed plate, rotation axis and rotation
It is flexibly connected between plate by the second angular displacement sensor；First angular displacement sensor and the second angular displacement sensor with control
Device is electrically connected, and is connected with wireless transport module on controller.
Further, it is provided with gap between fixed gear and pedal base, is provided between fixed gear and pedal base multiple
Position spring, and reset spring is fixed in the fixed column being arranged in pedal base.
Further, damping spring is provided between rotor plate and fixed plate, the both ends of damping spring pass through connecting column point
It is not fixed on rotor plate and fixed plate.
Further, limit hole is offered on rotor plate, stop collar corresponding with limit hole is provided in fixed plate, is limited
Bolt is provided in ring and limit hole.
Further, fixed plate is " H " shape structure, and the bottom at four angles of fixed plate is provided with idler wheel.
Further, the center of fixed plate is arranged in rotation axis, and the second angular displacement sensor is located at the center of rotor plate.
Further, the front and rear ends of pedal are provided with Antiskid platform, and the rear end of pedal is provided with baffle.
Further, the lower end of rotor plate is provided with arc-shaped sliding slot, is provided in insertion sliding slot above fixed plate
Slide post, slide post is slidably connected with sliding slot, and the center of circle of sliding slot is the tie point of rotation axis and rotor plate.
The invention has the benefit that this programme applied to unmanned plane manipulate, staff by both feet to unmanned plane into
The operations such as row yaw, steering and inclination；In use, both feet are individually positioned on two pedals, two are trampled by control and is stepped on
The different dynamics of plate controls the revolving speed of left and right two engines of unmanned plane respectively, and then unmanned plane is tilted and turned to
Operation, pedal rotate forward around hinge joint, and the induction gear in pedal base is around fixed gear rotation, the first angle displacement transducer
The angular displacement that device will test is exported by electric signal, and is handled by controller, issues control instruction to unmanned plane；Rotor plate can
The angular displacement for rotating around fixed plate, and being relatively rotated by the second Angular Displacement Detecting, corrects the yaw of unmanned plane.
Reset spring provides certain damping for resetting to pedal when pushes pedals, increases operation
Sense；Damping spring provides certain damping for resetting to rotor plate, and during rotor plate rotation, increases operation
Sense；Hole and stop collar are limited for limiting to rotor plate and fixed plate, under conventional non-operation state, bolt locks rotation
Plate and fixed plate prevent from rotating；Idler wheel in fixed plate facilitates entire pedal mobile；Baffle on pedal facilitates foot to be placed on pedal
On, it avoids skidding；When rotor plate is rotated around fixed plate, slide post slides in sliding slot, increases the stability of rotation, avoids out
Now deviate.
Detailed description of the invention
Fig. 1 is the front view that unmanned plane manipulates pedal.
Fig. 2 is the bottom view that unmanned plane manipulates pedal.
Fig. 3 is the structural schematic diagram inside pedal base.
Wherein, 1, fixed plate, 2, sliding slot, 3, connecting column, 4, damping spring, 5, rotor plate, 6, stop collar, 7, limit hole,
8, rotation axis, 9, baffle, 10, idler wheel, 11, strip groove, 12, pedal base, 13, induction gear, 14, fixation gear, 15, fixation
Column, 16, reset spring, the 17, second angular displacement sensor, 18, pedal.
Specific embodiment
A specific embodiment of the invention is described below, in order to facilitate understanding by those skilled in the art this hair
It is bright, it should be apparent that the present invention is not limited to the ranges of specific embodiment, for those skilled in the art,
As long as various change is in the spirit and scope of the present invention that the attached claims limit and determine, these variations are aobvious and easy
See, all are using the innovation and creation of present inventive concept in the column of protection.
As shown in Figure 1 to Figure 3, the rotor plate 5 of unmanned plane manipulation pedal including " H " shape, opens up that there are two items on rotor plate 5
Shape slot 11, two strip grooves 11 are located at the left and right sides of rotor plate 5；It is provided with pedal base 12 in two strip grooves 11,
It is provided with pedal 18 on pedal base 12, is arcuate structure below pedal base 12；Fixed fixation gear is provided in strip groove 11
14, and fixed gear 14 passes through pedal base 12, and extends into pedal base 12；Between having between fixed gear 14 and pedal base 12
Gap is provided with induction gear 13 in pedal base 12, and induction gear 13 is mounted on pedal base 12 by the first angular displacement sensor
It is interior；Pedal base 12 is hinged on fixed gear 14, and induction gear 13 is engaged with fixed gear 14.
5 underside of rotor plate is provided with fixed plate 1, is connected between fixed plate 1 and rotor plate 5 by rotation axis 8, and turns
Moving axis 8 is fixed in fixed plate 1, is rotatablely connected between rotation axis 8 and rotor plate 5 by the second angular displacement sensor 17；First
Angular displacement sensor and the second angular displacement sensor 17 are electrically connected with the controller, and wireless transport module is provided on controller；
Controller uses C51 single-chip microcontroller, and wireless transport module uses USR-G780V2 type wireless transport module.
This programme is manipulated applied to unmanned plane, and staff yaws unmanned plane, turns to and tilted by both feet
Operation；In use, both feet are individually positioned on two pedals 18, two different dynamics of pedal 18 are trampled by control, point
Not come the revolving speed for controlling left and right two engines of unmanned plane, and then inclination and steering operation are carried out to unmanned plane.
Pedal 18 rotates forward around hinge joint, and the induction gear 13 in pedal base 12 is rotated around fixed gear 14, the
The angular displacement that one angular displacement sensor will test is exported by electric signal, and is handled by controller, is issued and is controlled to unmanned plane
Instruction；Rotor plate 5 can be rotated around fixed plate 1, and the angular displacement relatively rotated by the second Angular Displacement Detecting, correct unmanned plane
Yaw.First angular displacement sensor and the second angular displacement sensor 17 are all made of DWQT type 4-20mA electric current angle displacement sensing
Device.
As shown in figure 3, gap is provided between fixed gear 14 and pedal base 12, between fixed gear 14 and pedal base 12
It is provided with reset spring 16, and reset spring 16 is fixed in the fixed column 15 in pedal base 12.Reset spring 16 is used for stepping on
Plate 18 is resetted, and certain damping is provided when pushes pedals 18, increases operation sense；Reset spring 16 is in normal
When length, pedal 18 is not trampled, and the angular displacement of the first angular displacement sensor detection is 0.
Damping spring 4 is provided between rotor plate 5 and fixed plate 1, the both ends of damping spring 4 are solid respectively by connecting column 3
It is scheduled on rotor plate 5 and fixed plate 1.Damping spring 4 is used to reset rotor plate 5, and during rotor plate 5 rotates
Certain damping is provided, operation sense is increased；When damping sensor is in normal length, rotor plate 5 is completely coincident with fixed plate 1,
The angle that rotor plate 5 rotates is 0.
Offered on rotor plate 5 and limit hole, be provided with stop collar 6 corresponding with limit hole 7 in fixed plate 1, stop collar 6 with
Bolt is provided in limit hole 7.It limits hole and stop collar 6 is used for that fixed plate 1 to rotor plate 5 limits, and not to grasp routinely
Under vertical state, limits hole and stop collar 6 is inserted into bolt, lock rotor plate 5 and fixed plate 1, prevent from rotating.
Fixed plate 1 is " H " shape structure, and the bottom at 1 four angles of fixed plate is provided with idler wheel 10, the idler wheel 10 in fixed plate 1
Facilitate entire pedal mobile.The center of fixing seat is arranged in rotation axis 8, and the second angular displacement sensor 17 is located in rotor plate 5
Centre.
The front and rear ends of pedal 18 are provided with Antiskid platform, and the rear end of pedal 18 is provided with baffle 9；The lower end of rotor plate 5
It is provided with arc-shaped sliding slot 2, the top of fixed plate 1 is provided with the slide post in insertion sliding slot 2, and slide post and sliding slot 2 slide
Connection, the center of circle of sliding slot 2 are the tie point of rotation axis 8 and rotor plate 5.Baffle 9 on pedal 18 facilitates foot to be placed on pedal 18,
It avoids skidding；When rotor plate 5 is rotated around fixed plate 1, slide post slides in sliding slot 2, increases the stability of rotation, avoids out
Now deviate.
Claims (8)
1. a kind of unmanned plane manipulates pedal, which is characterized in that the rotor plate (5) including " H " shape opens up on the rotor plate (5)
There are two strip groove (11), it is provided with pedal base (12) on two strip grooves (11), is arranged on the pedal base (12)
Have pedal (18), be provided with fixed gear (14) in the strip groove (11), and fixed gear (14) extend into pedal base (12)
It is interior, it is provided with induction gear (13) in the pedal base (12), and induction gear (13) is installed by the first angular displacement sensor
On pedal base (12)；The pedal base (12) is hinged on fixed gear (14), the induction gear (13) and fixed gear
(14) it engages；
It is connected with fixed plate (8) below the rotor plate (5) by rotation axis (8), and rotation axis (8) is fixed on fixed plate (1)
On, it is flexibly connected between the rotation axis (8) and rotor plate (5) by the second angular displacement sensor (17)；First jiao of position
Displacement sensor and the second angular displacement sensor (17) are electrically connected with the controller, and wireless transmission mould is connected on the controller
Block.
2. unmanned plane according to claim 1 manipulates pedal, which is characterized in that the fixed gear (14) and pedal base
(12) it is provided with gap between, is provided with reset spring (16) between the fixed gear (14) and pedal base (12), and resets
Spring (16) is fixed in the fixed column (15) being arranged in pedal base (12).
3. unmanned plane according to claim 1 manipulates pedal, which is characterized in that the rotor plate (5) and fixed plate (1) it
Between be provided with damping spring (4), the both ends of the damping spring (4) are separately fixed at rotor plate (5) by connecting column (3) and consolidate
On fixed board (1).
4. unmanned plane according to claim 1 manipulates pedal, which is characterized in that offer limit on the rotor plate (5)
Hole (7) is provided with stop collar (6) corresponding with limit hole (7), the stop collar (6) and limit hole on the fixed plate (1)
(7) bolt is provided in.
5. unmanned plane according to claim 1 manipulates pedal, which is characterized in that the fixed plate (1) is " H " shape structure,
The bottom at (1) four angle of fixed plate is provided with idler wheel (10).
6. unmanned plane according to claim 1 manipulates pedal, which is characterized in that the rotation axis (8) is arranged in fixed plate
(1) center, second angular displacement sensor (17) are located at the center of rotor plate (5).
7. unmanned plane according to claim 1 manipulates pedal, which is characterized in that the front and rear ends of the pedal (18) are equal
It is provided with Antiskid platform, the rear end of the pedal (18) is provided with baffle (9).
8. unmanned plane according to claim 1 manipulates pedal, which is characterized in that the lower end of the rotor plate (5) is provided with
Arc-shaped sliding slot (2), the slide post being provided with above the fixed plate (1) in insertion sliding slot (2), the slide post and cunning
Slot (2) is slidably connected, and the center of circle of the sliding slot (2) is the tie point of rotation axis (8) and rotor plate (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910461831.1A CN110109507A (en) | 2019-05-30 | 2019-05-30 | A kind of unmanned plane manipulation pedal |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910461831.1A CN110109507A (en) | 2019-05-30 | 2019-05-30 | A kind of unmanned plane manipulation pedal |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110109507A true CN110109507A (en) | 2019-08-09 |
Family
ID=67492960
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910461831.1A Pending CN110109507A (en) | 2019-05-30 | 2019-05-30 | A kind of unmanned plane manipulation pedal |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110109507A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103605400A (en) * | 2013-11-27 | 2014-02-26 | 连云港杰瑞电子有限公司 | Pedal controller |
| KR101549107B1 (en) * | 2014-09-02 | 2015-09-02 | 재단법인 실감교류인체감응솔루션연구단 | Apparatus for interacting with external device by using scaffolding module |
| CN208314607U (en) * | 2018-03-01 | 2019-01-01 | 中国航空无线电电子研究所 | Adjustable unmanned plane pedal |
| CN109407750A (en) * | 2018-12-27 | 2019-03-01 | 宁波慈溪小家电创新设计研究院有限公司 | A kind of foot rudder |
| CN209674268U (en) * | 2019-05-30 | 2019-11-22 | 成都航空职业技术学院 | A kind of unmanned plane manipulation pedal |
-
2019
- 2019-05-30 CN CN201910461831.1A patent/CN110109507A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103605400A (en) * | 2013-11-27 | 2014-02-26 | 连云港杰瑞电子有限公司 | Pedal controller |
| KR101549107B1 (en) * | 2014-09-02 | 2015-09-02 | 재단법인 실감교류인체감응솔루션연구단 | Apparatus for interacting with external device by using scaffolding module |
| CN208314607U (en) * | 2018-03-01 | 2019-01-01 | 中国航空无线电电子研究所 | Adjustable unmanned plane pedal |
| CN109407750A (en) * | 2018-12-27 | 2019-03-01 | 宁波慈溪小家电创新设计研究院有限公司 | A kind of foot rudder |
| CN209674268U (en) * | 2019-05-30 | 2019-11-22 | 成都航空职业技术学院 | A kind of unmanned plane manipulation pedal |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN209674268U (en) | A kind of unmanned plane manipulation pedal | |
| US8774983B2 (en) | Towbarless airplane tug | |
| US9022317B2 (en) | Towbarless airplane tug | |
| US10005489B2 (en) | Ratchet assembly and rotational sensor drive mechanism | |
| US20070124034A1 (en) | Method for checking takeoff or landing parameters, and associated device | |
| CN201551845U (en) | Flight assisting system for model airplane with fixed wings | |
| CN206087287U (en) | Express delivery unmanned aerial vehicle | |
| KR20100040802A (en) | Towbarless airplane tug | |
| CN106629525A (en) | Rotation device capable of automatically limiting rotation angle of working platform, and control method | |
| CN109204604B (en) | A kind of Intelligent Mobile Robot aiding overpass obstacle system and method | |
| CN110109507A (en) | A kind of unmanned plane manipulation pedal | |
| WO2016048437A1 (en) | Initial rotor state compensation for a rotorcraft | |
| CN208488103U (en) | A kind of magnetic compass correction simulator | |
| RU2350905C2 (en) | Method and device for measurement of aircraft nose chassis orientation | |
| CN205998050U (en) | The vehicles | |
| CN205138614U (en) | Road vehicle intelligence dynamic weighing system | |
| CN209305838U (en) | Multi-rotor unmanned aerial vehicle recyclable device | |
| SE504617C2 (en) | Methods and apparatus for controlling a passenger bridge | |
| JP7140417B2 (en) | drone system | |
| CN203780426U (en) | Rolling ladder control mechanism for corn machine | |
| AU2021286313A1 (en) | Telehandler with facilitated alignment adjustment | |
| CN109018414A (en) | Helicopter Slope Auxiliary Landing System | |
| CN108664041B (en) | Aircraft tilting angle detection device, control system and method | |
| CN103770714B (en) | Corn machine turns terraced steering unit | |
| CN109625080A (en) | Electric-controlled hydraulic steering system, autocrane, electric-controlled hydraulic rotating direction control method |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |