CN105278538A - Device and method of remote control of unmanned aerial vehicle with aeroplane heading indication - Google Patents
Device and method of remote control of unmanned aerial vehicle with aeroplane heading indication Download PDFInfo
- Publication number
- CN105278538A CN105278538A CN201510819716.9A CN201510819716A CN105278538A CN 105278538 A CN105278538 A CN 105278538A CN 201510819716 A CN201510819716 A CN 201510819716A CN 105278538 A CN105278538 A CN 105278538A
- Authority
- CN
- China
- Prior art keywords
- remote control
- display device
- type display
- sensor
- unmanned plane
- 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.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims abstract description 23
- 230000001133 acceleration Effects 0.000 claims description 13
- 230000005484 gravity Effects 0.000 claims description 11
- 230000004888 barrier function Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000012800 visualization Methods 0.000 description 1
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The present invention discloses a device and method of remote control of an unmanned aerial vehicle with an aeroplane heading indication. The device provided by the invention comprises a main body of a remote control device, a left remote control lever and a right remote control lever. The device of the remote control further comprises: a sensor configured to detect the attitude of the remote control device; a processing control chip configured to receive attitude information and satellite positioning information and perform data process of received information so as to obtain the position, the angle, and the speed of the unmanned aerial vehicle relative to the remote control device; a left circular display device and a right circular device provided with a plurality of circular light point indication units configured for lightening; and a display control chip configured to connect with the sensor, the processing control chip, the left circular display device and the right circular display device and control the lightening of the circular light point indication units on the left circular display device and the right circular device and the indication of the aeroplane heading of the unmanned aerial vehicle. According to the invention, the orientation of the aeroplane heading of an unmanned aerial vehicle may be visually, rapidly and accurately determined.
Description
Technical field
The present invention relates to no-manned machine distant control device, in particular a kind of no-manned machine distant control device and method with heading instruction.
Background technology
In prior art, some no-manned machine distant control devices only can rely on visualization to judge the heading of unmanned plane in use, when over the horizon is flown, heading just becomes and is difficult to determine, user, in the controlling once to heading error in judgement, is easy to cause unmanned plane off-course even to be bumped against with barrier.Current production majority all uses Airborne Camera that Image Real-time Transmission is returned remote control end, judges Handpiece Location by the picture observing shooting, and this kind of method exists that real-time is poor, operator is difficult to the problems such as accurately judgement when being unfamiliar with picture mesorelief.
Therefore, prior art existing defects, needs to improve.
Summary of the invention
Technical matters to be solved by this invention is: provide a kind of can judge intuitively, quickly and accurately unmanned plane head towards band heading instruction no-manned machine distant control device and method.
Technical scheme of the present invention is as follows: a kind of no-manned machine distant control device with heading instruction, comprise remote control system main body, left remote control rod and right remote control rod, it is characterized in that: also comprise: be arranged on the sensor detected in remote control system main body and to the attitude of telechiric device; Be arranged in remote control system main body, for receiving the attitude information of unmanned plane and satellite positioning information and carrying out data processing to the information received, obtain the processing controls chip of the relative position of unmanned plane and telechiric device, angle, speed; Be separately positioned on the left ring-type display device around left remote control rod and right remote control rod and right ring-type display device, left ring-type display device and right ring-type display device are respectively arranged with some electroluminescent lamp points for lighting; Be connected with processing controls chip, left ring-type display device and right ring-type display device respectively, and light for the electroluminescent lamp point that the relative position of the attitude according to telechiric device, unmanned plane and telechiric device, angle, speed control in left ring-type display device and right ring-type display device and indicate the display control chip of unmanned plane heading.
Be applied to technique scheme, in described no-manned machine distant control device, sensor setting is the one or several arbitrarily in electronic compass sensor or acceleration transducer or gravity sensor or satnav sensor.
Be applied to each technique scheme, in described no-manned machine distant control device, electroluminescent lamp point is set to monochromatic LED pilot lamp point or multi-colored led pilot lamp point.
Be applied to each technique scheme, a kind of no-manned machine distant control method with heading instruction, comprises the steps: A: detected by the attitude of sensor to telechiric device, obtain the attitude information of telechiric device; B: by receiving the attitude information of unmanned plane and satellite positioning information and carrying out data processing to the information received, obtain the relative position of unmanned plane and telechiric device, angle and speed; C: according to relative position, angle, the speed of the attitude information of telechiric device, unmanned plane and telechiric device, generates display control signal; D: telechiric device is according to the heading of display control signal instruction unmanned plane.
Be applied to each technique scheme, in described no-manned machine distant control method, in steps A: be detect by arranging the attitude of sensor to telechiric device in the remote control system main body of telechiric device.
Be applied to each technique scheme, in described no-manned machine distant control method, sensor setting is the one or several arbitrarily in electronic compass sensor or acceleration transducer or gravity sensor or satnav sensor.
Be applied to each technique scheme, in described no-manned machine distant control method, in step D, by arranging left ring-type display device and right ring-type display device respectively around the left remote control rod and right remote control rod of telechiric device, and the heading indicating unmanned plane for the some electroluminescent lamp points lighted by left ring-type display device and right ring-type display device are arranged respectively.
Adopt such scheme, the present invention by arranging sensor, processing controls chip and ring-type display device in telechiric device, the heading of unmanned plane is obtained by sensor and processing controls chip, and shown intuitively by ring-type display device, the judgement of relative Handpiece Location becomes more simple.
Accompanying drawing explanation
Fig. 1 is syndeton schematic diagram of the present invention;
Fig. 2 be in the present invention unmanned plane head towards the structural representation in telepilot dead ahead;
Fig. 3 be in the present invention unmanned plane head towards the structural representation of telepilot left front.
Embodiment
Below in conjunction with the drawings and specific embodiments, the present invention is described in detail.
Present embodiments provide a kind of no-manned machine distant control device with heading instruction, as shown in 1-3, no-manned machine distant control device comprises remote control system main body 1, left remote control rod 22 and right remote control rod 21, and, in remote control system main body, be also provided with the sensor that the attitude of telechiric device is detected; Sensor can be electronic compass sensor or acceleration transducer or gravity sensor or satnav sensor, or, sensor can be any two kinds or combinations two or more arbitrarily in electronic compass sensor or acceleration transducer or gravity sensor or satnav sensor, wherein, attitude refers to the positional information, acceleration of gravity information, acceleration information, directional information etc. of the telechiric device got by sensor.
And, remote control system main body is also arranged on a processing controls chip, processing controls chip and unmanned plane wireless connections, unmanned plane is while flight, the attitude information flown and satellite positioning information are wirelessly sent to processing controls chip, processing controls chip carries out data processing to its information received, by calculating the relative position of unmanned plane and telechiric device, angle and speed.
As shown in Figures 2 and 3, left ring-type display device 32 is provided with around left remote control rod 22, right ring-type display device 31 is provided with around right remote control rod 21, left ring-type display device 32 and left ring-type display device are respectively arranged with some electroluminescent lamp points 4 for lighting, and electroluminescent lamp point 4, by some monochromatic LED lamps or Multicolor LED lamp point, is mutually arranged in ring-type and forms, so, by monochromatic LED lamp or Multicolor LED lamp point, by arranging and controlling, not homochromy light can be sent.
And, the present embodiment additionally provides a kind of no-manned machine distant control method with heading instruction, comprise the steps: first, steps A: detecting by being arranged on the attitude of the sensor in remote control system main body to telechiric device, obtaining the attitude information of telechiric device; Sensor can be electronic compass sensor or acceleration transducer or gravity sensor or satnav sensor, or, sensor can be any two kinds or combinations two or more arbitrarily in electronic compass sensor or acceleration transducer or gravity sensor or satnav sensor, wherein, attitude refers to the positional information, acceleration of gravity information, acceleration information, directional information etc. of the telechiric device got by sensor.
Then, step B: can in telechiric device set handling control chip, processing controls chip and unmanned plane wireless connections, unmanned plane is while flight, the attitude information flown and satellite positioning information are wirelessly sent to processing controls chip, processing controls chip carries out data processing to its information received, by calculating the relative position of unmanned plane and telechiric device, angle and speed.
Then step C is performed: namely can by arranging display control chip, by relative position, angle, the speed of display control chip according to the attitude information of telechiric device, unmanned plane and telechiric device, generation display control signal; In step D, telechiric device is according to the heading of display control signal instruction unmanned plane finally.Wherein, in step D, by arranging left ring-type display device and left ring-type display device respectively around the left remote control rod and right remote control rod of telechiric device, and the heading indicating unmanned plane for the electroluminescent lamp point indicating member lighted by left ring-type display device and left ring-type display device are arranged respectively, electroluminescent lamp point 4 by monochromatic LED or multi-colored led pilot lamp, mutually be arranged in ring-type to form, so, by some monochromatic LEDs or multi-colored led pilot lamp, by arranging and controlling, different light can be sent.
So, the present embodiment is by a kind of telepilot no-manned machine distant control device with heading instruction of design, this device installs a loop display device at the control lever periphery of remote control equipment, and in use this ring-type display device can indicate heading by light.Be that left remote control rod controls unmanned plane course shown in accompanying drawing 2 and 3, different according to operating habit, left remote-control lever and right remote control rod, left ring-type display device and left ring-type display device functionalities can switch mutually.
First, the first step increases sensor (including but not limited to electronic compass, acceleration transducer, gravity sensor, global position system etc.) on the remote control device, realizes the attitude detection to remote controller.
Then, the attitude information of unmanned plane, satellite positioning information etc. are back to telechiric device by radio by second step, processing controls chip in telechiric device can process data, obtains the information such as the relative position of unmanned plane and telechiric device, angle, speed.
This information is displayed by left ring-type display device and left ring-type display device by the 3rd step, and as in Fig. 1, unmanned plane head 5 is towards telepilot dead ahead, then lamplight pointing unit 4 is presented at the dead ahead of direction rocking bar.When unmanned plane heading changes, as Fig. 2, then lamplight pointing unit 4 also can change thereupon.Finally can realize regardless of telechiric device and unmanned plane towards, lamplight pointing unit 4 accurately can both demonstrate the accurate Handpiece Location of unmanned plane relative to telechiric device.Left ring-type display device and left ring-type display device also can show the pattern of different color, shape, and the operation readiness that can be used for unmanned plane is also guided or shows the information such as state of flight, electricity, speed of unmanned plane.
These are only preferred embodiment of the present invention, be not limited to the present invention, all any amendments done within the spirit and principles in the present invention, equivalent replacement and improvement etc., all should be included within protection scope of the present invention.
Claims (7)
1. the no-manned machine distant control device with heading instruction, comprises remote control system main body, left remote control rod and right remote control rod, it is characterized in that:
Also comprise:
Be arranged on the sensor detected in remote control system main body and to the attitude of telechiric device;
Be arranged in remote control system main body, for receiving the attitude information of unmanned plane and satellite positioning information and carrying out data processing to the information received, obtain the processing controls chip of the relative position of unmanned plane and telechiric device, angle, speed;
Be separately positioned on the left ring-type display device around left remote control rod and right remote control rod and right ring-type display device, left ring-type display device and right ring-type display device are respectively arranged with some electroluminescent lamp points for lighting;
Be connected with processing controls chip, left ring-type display device and right ring-type display device respectively, and light for the electroluminescent lamp point that the relative position of the attitude according to telechiric device, unmanned plane and telechiric device, angle, speed control in left ring-type display device and right ring-type display device and indicate the display control chip of unmanned plane heading.
2. no-manned machine distant control device according to claim 1, is characterized in that: sensor setting is the one or several arbitrarily in electronic compass sensor or acceleration transducer or gravity sensor or satnav sensor.
3. no-manned machine distant control device according to claim 1, is characterized in that: electroluminescent lamp point is set to monochromatic LED pilot lamp point or multi-colored led pilot lamp point.
4. the no-manned machine distant control method with heading instruction, comprises the steps:
A: detected by the attitude of sensor to telechiric device, obtain the attitude information of telechiric device;
B: by receiving the attitude information of unmanned plane and satellite positioning information and carrying out data processing to the information received, obtain the relative position of unmanned plane and telechiric device, angle and speed;
C: according to relative position, angle, the speed of the attitude information of telechiric device, unmanned plane and telechiric device, generates display control signal;
D: telechiric device is according to the heading of display control signal instruction unmanned plane.
5. no-manned machine distant control method according to claim 4, is characterized in that: in steps A: be detect by arranging the attitude of sensor to telechiric device in the remote control system main body of telechiric device.
6. no-manned machine distant control method according to claim 5, is characterized in that: sensor setting is the one or several arbitrarily in electronic compass sensor or acceleration transducer or gravity sensor or satnav sensor.
7. no-manned machine distant control method according to claim 4, it is characterized in that: in step D, by arranging left ring-type display device and right ring-type display device respectively around the left remote control rod and right remote control rod of telechiric device, and the heading indicating unmanned plane for the some electroluminescent lamp points lighted by left ring-type display device and right ring-type display device are arranged respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510819716.9A CN105278538B (en) | 2015-11-24 | 2015-11-24 | A kind of no-manned machine distant control device and method indicated with heading |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510819716.9A CN105278538B (en) | 2015-11-24 | 2015-11-24 | A kind of no-manned machine distant control device and method indicated with heading |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105278538A true CN105278538A (en) | 2016-01-27 |
| CN105278538B CN105278538B (en) | 2017-11-07 |
Family
ID=55147718
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510819716.9A Active CN105278538B (en) | 2015-11-24 | 2015-11-24 | A kind of no-manned machine distant control device and method indicated with heading |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105278538B (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106023554A (en) * | 2016-06-17 | 2016-10-12 | 深圳市元征科技股份有限公司 | Remote control method and remote controller |
| CN106292799A (en) * | 2016-08-25 | 2017-01-04 | 北京奇虎科技有限公司 | Unmanned plane, remote control unit and control method thereof |
| CN111189534A (en) * | 2020-01-13 | 2020-05-22 | 长沙矿山研究院有限责任公司 | Method for improving accuracy of aligning blasting vibration meter sensor to blasting core |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102650884A (en) * | 2011-02-25 | 2012-08-29 | 鸿富锦精密工业（深圳）有限公司 | Controller and method for adjusting control signals by utilizing controller |
| US20140142784A1 (en) * | 2012-03-14 | 2014-05-22 | Prox Dynamics As | Control of uav |
| CN203996914U (en) * | 2014-07-04 | 2014-12-10 | 深圳市嘉兰图设计有限公司 | A kind of four-axle aircraft backward direction indicating system |
| CN204219780U (en) * | 2014-10-11 | 2015-03-25 | 广东信宇科技实业有限公司 | A kind of remote controller of toy car |
| CN204319768U (en) * | 2014-11-19 | 2015-05-13 | 甘甜田 | A kind of aircraft remote control equipment |
| CN205193595U (en) * | 2015-11-24 | 2016-04-27 | 深圳飞马机器人科技有限公司 | Unmanned aerial vehicle remote control unit of tape unit head direction indication |
-
2015
- 2015-11-24 CN CN201510819716.9A patent/CN105278538B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102650884A (en) * | 2011-02-25 | 2012-08-29 | 鸿富锦精密工业（深圳）有限公司 | Controller and method for adjusting control signals by utilizing controller |
| US20140142784A1 (en) * | 2012-03-14 | 2014-05-22 | Prox Dynamics As | Control of uav |
| CN203996914U (en) * | 2014-07-04 | 2014-12-10 | 深圳市嘉兰图设计有限公司 | A kind of four-axle aircraft backward direction indicating system |
| CN204219780U (en) * | 2014-10-11 | 2015-03-25 | 广东信宇科技实业有限公司 | A kind of remote controller of toy car |
| CN204319768U (en) * | 2014-11-19 | 2015-05-13 | 甘甜田 | A kind of aircraft remote control equipment |
| CN205193595U (en) * | 2015-11-24 | 2016-04-27 | 深圳飞马机器人科技有限公司 | Unmanned aerial vehicle remote control unit of tape unit head direction indication |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106023554A (en) * | 2016-06-17 | 2016-10-12 | 深圳市元征科技股份有限公司 | Remote control method and remote controller |
| CN106292799A (en) * | 2016-08-25 | 2017-01-04 | 北京奇虎科技有限公司 | Unmanned plane, remote control unit and control method thereof |
| CN111189534A (en) * | 2020-01-13 | 2020-05-22 | 长沙矿山研究院有限责任公司 | Method for improving accuracy of aligning blasting vibration meter sensor to blasting core |
| CN111189534B (en) * | 2020-01-13 | 2020-12-25 | 长沙矿山研究院有限责任公司 | Method for improving accuracy of aligning blasting vibration meter sensor to blasting core |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105278538B (en) | 2017-11-07 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11899472B2 (en) | Aerial vehicle video and telemetric data synchronization | |
| US10648809B2 (en) | Adaptive compass calibration based on local field conditions | |
| CN105270399B (en) | The device and method thereof of vehicle are controlled using vehicle communication | |
| US20160327389A1 (en) | Calibration Transfer Between Two Devices | |
| CN107085433B (en) | Light emission control device, unmanned aerial vehicle, and light emission control method | |
| EP3299920B1 (en) | Unmanned aerial vehicle control method and device based on no-head mode | |
| CN107289931B (en) | A kind of methods, devices and systems positioning rigid body | |
| JP2007155699A (en) | Mobile robot positioning system, and method using camera and indicator | |
| CN108253966B (en) | Three-dimensional simulation display method for flight of unmanned aerial vehicle | |
| NO20120341A1 (en) | Method and apparatus for controlling and monitoring the surrounding area of an unmanned aircraft | |
| KR102083934B1 (en) | Method and apparaus for automatic landing of aircraft using vision-based information | |
| KR101408077B1 (en) | An apparatus and method for controlling unmanned aerial vehicle using virtual image | |
| CN105739514A (en) | Operation and control method of unmanned aerial vehicle and unmanned aerial vehicle system | |
| CN103675609A (en) | Power line patrol equipment and system | |
| US10882637B1 (en) | Systems and methods for search and rescue light control for a rotorcraft | |
| CN105278538A (en) | Device and method of remote control of unmanned aerial vehicle with aeroplane heading indication | |
| KR101914179B1 (en) | Apparatus of detecting charging position for unmanned air vehicle | |
| JP2017105429A (en) | Unmanned flight body and control method for flight thereof | |
| JP2014220604A (en) | Photographing position information display device | |
| JP2017144988A (en) | Light emission control device, unmanned flight body, and light emission control method | |
| JP2019032234A (en) | Display device | |
| CN205193595U (en) | Unmanned aerial vehicle remote control unit of tape unit head direction indication | |
| CN107077144B (en) | Method, system and control device for displaying state of movable device | |
| JP2008252643A (en) | Mobile monitoring system and monitoring method thereof | |
| US10102741B2 (en) | Remote control device for aircraft, aircraft system and remote control method for aircraft system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: 518000, 1st Floor, 16th Building, Zhiheng Industrial Park, Nantou Street, Nanshan District, Shenzhen City, Guangdong Province Patentee after: Shenzhen Pegasus Robotics Co.,Ltd. Address before: 518000, 1st Floor, 16th Building, Zhiheng Industrial Park, Nantou Street, Nanshan District, Shenzhen City, Guangdong Province Patentee before: SHENZHEN FEIMA ROBOTICS Co.,Ltd. |
|
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: 518000, 13th Floor, Building A4, Nanshan Zhiyuan, No. 1001 Xueyuan Avenue, Changyuan Community, Taoyuan Street, Nanshan District, Shenzhen, Guangdong Province Patentee after: Shenzhen Pegasus Robotics Co.,Ltd. Country or region after: China Address before: 518000, 1st Floor, 16th Building, Zhiheng Industrial Park, Nantou Street, Nanshan District, Shenzhen City, Guangdong Province Patentee before: Shenzhen Pegasus Robotics Co.,Ltd. Country or region before: China |
|
| CP03 | Change of name, title or address |