CN105388906A - Height detection remote control for unmanned aerial vehicle (UAV) - Google Patents

Height detection remote control for unmanned aerial vehicle (UAV) Download PDF

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Publication number
CN105388906A
CN105388906A CN201510850669.4A CN201510850669A CN105388906A CN 105388906 A CN105388906 A CN 105388906A CN 201510850669 A CN201510850669 A CN 201510850669A CN 105388906 A CN105388906 A CN 105388906A
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CN
China
Prior art keywords
unmanned plane
telepilot
remote control
uav
air pressure
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
Application number
CN201510850669.4A
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Chinese (zh)
Inventor
陈梦洋
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Wuxi Miracle Science & Technology Co Ltd
Original Assignee
Wuxi Miracle Science & Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Wuxi Miracle Science & Technology Co Ltd filed Critical Wuxi Miracle Science & Technology Co Ltd
Priority to CN201510850669.4A priority Critical patent/CN105388906A/en
Publication of CN105388906A publication Critical patent/CN105388906A/en
Pending legal-status Critical Current

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Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/10Simultaneous control of position or course in three dimensions
    • G05D1/101Simultaneous control of position or course in three dimensions specially adapted for aircraft
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/56Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
    • G01C19/5705Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using masses driven in reciprocating rotary motion about an axis
    • GPHYSICS
    • G08SIGNALLING
    • G08CTRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
    • G08C17/00Arrangements for transmitting signals characterised by the use of a wireless electrical link
    • G08C17/02Arrangements for transmitting signals characterised by the use of a wireless electrical link using a radio link

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Measuring Fluid Pressure (AREA)

Abstract

The invention discloses a height detection remote control for an unmanned aerial vehicle (UAV). The height detection remote control comprises a control processing module. An air pressure sensor is connected onto the control processing module. The air pressure sensor detects air pressure data of a remote control and transmits the data to the control processing module. The control processing module communicates with a UAV through a wireless communication module of the remote control, receives the air pressure data of the UAV, and calculates the height difference between the UAV and the remote control based on the air pressure data of the remote control and the air pressure data of the UAV. In this way, the height detection remote control can detect the height difference between the remote control and the UAV according to air pressure and measure the relative height, and is safe and reliable and easy to use.

Description

Unmanned plane height detection telepilot
Technical field
The present invention relates to unmanned plane field, particularly relate to a kind of unmanned plane height detection telepilot.
Background technology
Some unmanned aerial vehicle (UAV) control modes mostly are remote pilot, and it needs all multiparameters beamed back according to unmanned plane to be judged whether voluntarily to be suitable for sending controling instruction by remote control manipulator.Current unmanned plane can locate the vertical range between unmanned plane to the earth by gps and sensor.But telepilot in the market can not detect the height of telepilot and aircraft, position residing for oneself can not be recognized in real time for mountain-climbing fan.
Summary of the invention
The technical matters that the present invention mainly solves is to provide a kind of unmanned plane height detection telepilot, can detect the difference in height of telepilot and unmanned plane according to air pressure, measures relative height, safe and reliable, easy to use.
For solving the problems of the technologies described above, the technical scheme that the present invention adopts is: provide a kind of unmanned plane height detection telepilot, comprise: control treatment module, described control treatment module is connected with baroceptor, described baroceptor detects the barometric information of telepilot, and send data to control treatment module, described control treatment module is by telepilot wireless communication module and UAV Communication, accept the barometric information of unmanned plane, and calculate the difference in height of unmanned plane and telepilot according to the barometric information of telepilot and the barometric information of unmanned plane.
In a preferred embodiment of the present invention, described unmanned plane comprises unmanned plane wireless communication module and unmanned plane baroceptor, and described unmanned plane baroceptor detects the air pressure of unmanned plane, is sent to telepilot by wireless communication module.
In a preferred embodiment of the present invention, described telepilot wireless communication module and unmanned plane wireless communication module are gps communication module.
The invention has the beneficial effects as follows: unmanned plane height detection telepilot of the present invention, the difference in height of telepilot and unmanned plane can be detected according to air pressure, measure relative height, safe and reliable, easy to use.
Accompanying drawing explanation
In order to be illustrated more clearly in the technical scheme in the embodiment of the present invention, below the accompanying drawing used required in describing embodiment is briefly described, apparently, accompanying drawing in the following describes is only some embodiments of the present invention, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings, wherein:
Fig. 1 is the structural representation of unmanned plane height detection telepilot one of the present invention preferred embodiment;
In accompanying drawing, the mark of each parts is as follows: 1, control treatment module, and 2, baroceptor, 3, wireless communication module, 4, unmanned plane, 5, unmanned plane wireless communication module, 6, unmanned plane baroceptor, 7, telepilot.
Embodiment
Be clearly and completely described to the technical scheme in the embodiment of the present invention below, obviously, described embodiment is only a part of embodiment of the present invention, instead of whole embodiments.Based on the embodiment in the present invention, those of ordinary skill in the art, not making other embodiments all obtained under creative work prerequisite, belong to the scope of protection of the invention.
Refer to Fig. 1, a kind of unmanned plane height detection telepilot, comprise: control treatment module 1, described control treatment module 1 is connected with baroceptor 2, described baroceptor 2 detects the barometric information of telepilot 7, and send data to control treatment module 1, described control treatment module 1 is communicated with unmanned plane 4 by telepilot wireless communication module 3, accept the barometric information of unmanned plane 4, and calculate the difference in height of unmanned plane 4 and telepilot 7 according to the barometric information of telepilot 7 and the barometric information of unmanned plane 4.
In addition, described unmanned plane 4 comprises unmanned plane wireless communication module 5 and unmanned plane baroceptor 6, and described unmanned plane baroceptor 5 detects the air pressure of unmanned plane, is sent to telepilot 7 by wireless communication module 6.
In addition, described telepilot wireless communication module 3 and unmanned plane wireless communication module 5 are gps communication module.
Unmanned plane height detection remote control appliance body running principle of the present invention is as follows: the telepilot baroceptor 2 on telepilot 7 detects the air pressure of telepilot 7, then barometric information is sent to control treatment module 1, unmanned plane baroceptor on unmanned plane detects the air pressure of 5 unmanned planes, and be sent to telepilot wireless communication module 2 by unmanned plane wireless communication module 4, telepilot wireless communication module 2 sends data to control treatment module 1, the vertical range both control treatment module 1 calculates according to the draught head of unmanned plane and telepilot.Unmanned plane can detect unmanned plane oneself height by the sensor that carries, and user can calculate sea level elevation residing for telepilot according to the difference in height of unmanned plane height and unmanned plane and telepilot.
Be different from prior art, unmanned plane height detection telepilot of the present invention, the difference in height of telepilot and unmanned plane can be detected according to air pressure, measure relative height, safe and reliable, easy to use.
The foregoing is only embodiments of the invention; not thereby the scope of the claims of the present invention is limited; every utilize description of the present invention to do equivalent structure or equivalent flow process conversion; or be directly or indirectly used in other relevant technical field, be all in like manner included in scope of patent protection of the present invention.

Claims (3)

1. a unmanned plane height detection telepilot, it is characterized in that, comprise: control treatment module, described control treatment module is connected with baroceptor, described baroceptor detects the barometric information of telepilot, and sends data to control treatment module, and described control treatment module is by telepilot wireless communication module and UAV Communication, accept the barometric information of unmanned plane, and calculate the difference in height of unmanned plane and telepilot according to the barometric information of telepilot and the barometric information of unmanned plane.
2. unmanned plane height detection telepilot according to claim 1, it is characterized in that, described unmanned plane comprises unmanned plane wireless communication module and unmanned plane baroceptor, and described unmanned plane baroceptor detects the air pressure of unmanned plane, is sent to telepilot by wireless communication module.
3. unmanned plane height detection telepilot according to claim 2, is characterized in that, described telepilot wireless communication module and unmanned plane wireless communication module are gps communication module.
CN201510850669.4A 2015-11-30 2015-11-30 Height detection remote control for unmanned aerial vehicle (UAV) Pending CN105388906A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510850669.4A CN105388906A (en) 2015-11-30 2015-11-30 Height detection remote control for unmanned aerial vehicle (UAV)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510850669.4A CN105388906A (en) 2015-11-30 2015-11-30 Height detection remote control for unmanned aerial vehicle (UAV)

Publications (1)

Publication Number Publication Date
CN105388906A true CN105388906A (en) 2016-03-09

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CN201510850669.4A Pending CN105388906A (en) 2015-11-30 2015-11-30 Height detection remote control for unmanned aerial vehicle (UAV)

Country Status (1)

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CN (1) CN105388906A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106952360A (en) * 2017-03-15 2017-07-14 览意科技(上海)有限公司 The unmanned plane of unmanned plane during flying online data collection method and application this method
CN107314756A (en) * 2016-12-15 2017-11-03 天津同创达科石油科技有限公司 Rig electronics anticollision system based on atmospheric pressure
WO2019037100A1 (en) * 2017-08-25 2019-02-28 SZ DJI Technology Co., Ltd. Altitude estimation for aerial vehicles
CN112164214A (en) * 2017-08-17 2021-01-01 深圳市大疆创新科技有限公司 Remote controller

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Publication number Priority date Publication date Assignee Title
CN201094017Y (en) * 2007-08-06 2008-07-30 樊生良 Atmospheric pressure altimeter
CN202632581U (en) * 2012-05-28 2012-12-26 戴震宇 Flight simulation control and experience device based on real air environment
CN202694151U (en) * 2011-12-16 2013-01-23 新时代集团国防科技研究中心 Control terminal device for unmanned aircraft
CN103019243A (en) * 2012-12-24 2013-04-03 杭州电子科技大学 Cross-flow fan based automatic navigation aircraft
US20130085629A1 (en) * 2011-09-30 2013-04-04 Aurora Flight Sciences Corporation Hardware-Based Weight And Range Limitation System, Apparatus And Method
CN103345826A (en) * 2013-07-05 2013-10-09 深圳市大疆创新科技有限公司 Remote control terminal of unmanned flight vehicle, as well as flight auxiliary system and method of unmanned flight vehicle
CN104536451A (en) * 2014-12-31 2015-04-22 深圳雷柏科技股份有限公司 Multi-rotor-wing aircraft with automatic stalling function after landing and control method
CN105045283A (en) * 2015-08-19 2015-11-11 无锡觅睿恪科技有限公司 Control unit of unmanned plane and operation interface thereof
CN105068556A (en) * 2015-07-16 2015-11-18 深圳市前海疆域智能科技股份有限公司 Aircraft automatic tracking method, mobile intelligent equipment, aircraft, and mobile intelligent system

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201094017Y (en) * 2007-08-06 2008-07-30 樊生良 Atmospheric pressure altimeter
US20130085629A1 (en) * 2011-09-30 2013-04-04 Aurora Flight Sciences Corporation Hardware-Based Weight And Range Limitation System, Apparatus And Method
CN202694151U (en) * 2011-12-16 2013-01-23 新时代集团国防科技研究中心 Control terminal device for unmanned aircraft
CN202632581U (en) * 2012-05-28 2012-12-26 戴震宇 Flight simulation control and experience device based on real air environment
CN103019243A (en) * 2012-12-24 2013-04-03 杭州电子科技大学 Cross-flow fan based automatic navigation aircraft
CN103345826A (en) * 2013-07-05 2013-10-09 深圳市大疆创新科技有限公司 Remote control terminal of unmanned flight vehicle, as well as flight auxiliary system and method of unmanned flight vehicle
CN104536451A (en) * 2014-12-31 2015-04-22 深圳雷柏科技股份有限公司 Multi-rotor-wing aircraft with automatic stalling function after landing and control method
CN105068556A (en) * 2015-07-16 2015-11-18 深圳市前海疆域智能科技股份有限公司 Aircraft automatic tracking method, mobile intelligent equipment, aircraft, and mobile intelligent system
CN105045283A (en) * 2015-08-19 2015-11-11 无锡觅睿恪科技有限公司 Control unit of unmanned plane and operation interface thereof

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107314756A (en) * 2016-12-15 2017-11-03 天津同创达科石油科技有限公司 Rig electronics anticollision system based on atmospheric pressure
CN106952360A (en) * 2017-03-15 2017-07-14 览意科技(上海)有限公司 The unmanned plane of unmanned plane during flying online data collection method and application this method
CN112164214A (en) * 2017-08-17 2021-01-01 深圳市大疆创新科技有限公司 Remote controller
CN112164214B (en) * 2017-08-17 2021-12-21 深圳市大疆创新科技有限公司 Remote controller
US11226617B2 (en) 2017-08-17 2022-01-18 SZ DJI Technology Co., Ltd. Remote control
WO2019037100A1 (en) * 2017-08-25 2019-02-28 SZ DJI Technology Co., Ltd. Altitude estimation for aerial vehicles
CN110621960A (en) * 2017-08-25 2019-12-27 深圳市大疆创新科技有限公司 Altitude estimation for aircraft
US11512953B2 (en) 2017-08-25 2022-11-29 SZ DJI Technology Co., Ltd. Altitude estimation for aerial vehicles

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Application publication date: 20160309