CN105527954A - Unmanned aerial vehicle remote control system - Google Patents

Unmanned aerial vehicle remote control system Download PDF

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Publication number
CN105527954A
CN105527954A CN201610070942.6A CN201610070942A CN105527954A CN 105527954 A CN105527954 A CN 105527954A CN 201610070942 A CN201610070942 A CN 201610070942A CN 105527954 A CN105527954 A CN 105527954A
Authority
CN
China
Prior art keywords
control
modular converter
signal
unmanned plane
signals
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
CN201610070942.6A
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Chinese (zh)
Inventor
郭齐红
张佩
杨永强
李超
林康
周权
祖金戈
汪连晖
张丽娇
孙阳
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.)
EAGLES MEN AERONAUTIC SCIENCE AND TECHNOLOGY GROUP Co Ltd
Original Assignee
EAGLES MEN AERONAUTIC SCIENCE AND TECHNOLOGY GROUP 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 EAGLES MEN AERONAUTIC SCIENCE AND TECHNOLOGY GROUP Co Ltd filed Critical EAGLES MEN AERONAUTIC SCIENCE AND TECHNOLOGY GROUP Co Ltd
Priority to CN201610070942.6A priority Critical patent/CN105527954A/en
Publication of CN105527954A publication Critical patent/CN105527954A/en
Pending legal-status Critical Current

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Classifications

    • 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
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B19/00Programme-control systems
    • G05B19/02Programme-control systems electric
    • G05B19/418Total factory control, i.e. centrally controlling a plurality of machines, e.g. direct or distributed numerical control [DNC], flexible manufacturing systems [FMS], integrated manufacturing systems [IMS], computer integrated manufacturing [CIM]
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P90/00Enabling technologies with a potential contribution to greenhouse gas [GHG] emissions mitigation
    • Y02P90/02Total factory control, e.g. smart factories, flexible manufacturing systems [FMS] or integrated manufacturing systems [IMS]

Abstract

The invention relates to the aviation control technology field, and particularly to an unmanned aerial vehicle remote control system. The unmanned aerial vehicle remote control system includes an electric device which controls an unmanned aerial vehicle. The electric device transmits network signals through an Ethernet control terminal and includes a third conversion module which converts the network signals into serial signals. The third conversion module transmits the serial signals to a fourth conversion module. The fourth conversion module converts the serial signals into control signals and transmits the control signals to a data transmission module. The data transmission module controls the unmanned aerial vehicle. The control terminal includes an operation handle which provides the control signals for a first conversion module. The first conversion module converts the control signals into the serial signals and transmits the serial signals to a second conversion module. The second conversion module converts the serial signals into the network signals and carries out signal communication with the third conversion module through an Ethernet. The control terminal includes an ARM processer and a 16-bit digital analog converter. The data time-delay of the control terminal is less than or equal to 200ms, the total power consumption is less than or equal to 10W, and the packet loss ratio is less than or equal to 0.5 per mill.

Description

A kind of unmanned plane tele-control system
Technical field
The present invention relates to aviation control technology field, be specifically related to a kind of unmanned plane tele-control system.
Background technology
In prior art, unmanned spacecraft UAV is called for short unmanned plane, and its volume is little, cost is low, good concealment, and be used to perform the tasks such as scouting, supervision and electronic interferences, combat success is striking.Along with the progress of science and technology and the change of strategic thought, unmanned plane will produce significant impact to future military action, and it will become the unmanned pioneer of battlefield main battle weaponry and the main force.Therefore strengthen the research work of unmanned plane, the military strength strengthening China is significant.
Chinese patent CN102183941 discloses a kind of ultra-long-range unmanned aerial vehicle control system based on civil mobile phone network, is made up of mobile system and ground system; Described mobile system is made up of communication navigation subsystem and gesture stability subsystem; Described communication navigation subsystem comprise Navigator is housed the first single-chip microcomputer, navigation module, the first servos control module, memory module, second singlechip, the second servos control module, mobile module, gang socket and sensor assembly; Described memory module is bi-directionally connected with described first single-chip microcomputer, described second singlechip respectively; The respective input of output termination first single-chip microcomputer of described navigation module, the corresponding output end of described first single-chip microcomputer connects the input end of the first servos control module; The respective input of the output termination second singlechip of described sensor assembly, the corresponding output end of described second singlechip connects the input end of the second servos control module; Described mobile module and gang socket are bi-directionally connected with described second singlechip respectively; Described gesture stability subsystem comprises the 3rd single-chip microcomputer, the 3rd servos control module, the first wireless data transfer module, height sensor, speed pickup and attachment plug; Described 3rd single-chip microcomputer is bi-directionally connected with described first wireless data transfer module, described attachment plug respectively, and the output terminal of described height sensor and speed pickup connects the respective input of described 3rd single-chip microcomputer respectively; Described ground system comprises computing machine, the second wireless data transfer module and game console, and described computing machine and the second wireless data transfer module are bi-directionally connected, the respective input of computing machine described in the output termination of described game console.But, this patent, the major way of current manual remote control is wireless remote control, but radio controlled longest distance only has about 800m; Autonomous flight does not rely on ground and controls, and all actions all can complete according to course line planned in advance automatically.Wireless remote control and autonomous flight can combinationally use by the modern times in-flight, can evade respective shortcoming, but command range is also just within 5km.Unmanned plane tele-control system command range disclosed by the invention is not by the impact of distance, and Long-distance Control just can be carried out to unmanned plane in the place that there is network.This technological breakthrough technical bottleneck of unmanned plane tele-control system, for unmanned plane Long-distance Control provides brand-new solution.
Summary of the invention
In order to overcome defect of the prior art, the present invention breaches the limit of unmanned plane Long-distance Control in distance, achieves thoroughly being separated of control terminal and unmanned aerial vehicle platform.
The present invention is achieved through the following technical solutions: a kind of unmanned plane tele-control system, comprise electronic equipment unmanned plane controlled by wireless signal, described electronic equipment carries out network signal transmission by Ethernet and control terminal, described electronic equipment comprises the 3rd modular converter network signal being converted to rs 232 serial interface signal, rs 232 serial interface signal is transferred to the 4th modular converter by described 3rd modular converter, described 4th modular converter converts the rs 232 serial interface signal of reception to control signal and is transferred to data transmission module, described data transmission module controls unmanned plane.
Further, described control terminal comprises the operating grip providing control signal to the first modular converter, described first modular converter converts the control signal received to rs 232 serial interface signal and is transferred to the second modular converter, and rs 232 serial interface signal is converted to network signal and carries out Signal transmissions communication by Ethernet and the 3rd modular converter by described second modular converter.
Further, described control terminal comprises the flight course planning display screen that carries out Signal transmissions with operating grip each other and The Cloud Terrace takes display screen.
Further, described control terminal comprises arm processor and 16 figure place weighted-voltage D/A converters.
Further, the data delay≤200ms of described control terminal, total power consumption≤10W, packet loss≤0.5 ‰.
Compared with prior art, superior effect is: the present invention breaches the limit of unmanned plane Long-distance Control in distance, achieves thoroughly being separated of control terminal and unmanned aerial vehicle platform.Be embodied in the following aspects:
(1) far distance controlled.Unmanned plane tele-control system command range is not by the impact of distance, and Long-distance Control just can be carried out to unmanned plane in the place that there is network;
(2) control accurately.Data delay≤the 200ms of unmanned plane tele-control system in the present invention, packet loss≤0.5 ‰, execute the task for the safety of newspaper unmanned plane and perfection and provide guarantee.
Long-distance Control unmanned plane scheme disclosed by the invention is not by the restriction of transmission range, and the transmission of control signal and image all keeps higher confidence level, plays larger impetus to the development of unmanned plane remote control technology.
Accompanying drawing explanation
Fig. 1 is the structured flowchart of unmanned plane tele-control system embodiment 1 of the present invention;
Fig. 2 is the structured flowchart of unmanned plane tele-control system embodiment 2 of the present invention.
Reference numeral is as follows:
1-unmanned plane, 2-control terminal, 3-electronic equipment, 4-flight course planning display screen, 5-The Cloud Terrace, 6-operating grip, 7-first modular converter, 8-second modular converter, 9-the 3rd modular converter, 10-the 4th modular converter, 11-data transmission module.
In figure, the direction of arrow is signal transmission direction.
Embodiment
Below in conjunction with accompanying drawing, the specific embodiment of the invention is described in further detail.
Embodiment 1
As shown in Figure 1, illustrate a kind of unmanned plane tele-control system provided by the invention, comprise the electronic equipment 3 unmanned plane 1 controlled by wireless signal, described electronic equipment 3 carries out network signal transmission by Ethernet and control terminal 2, described electronic equipment 3 comprises the 3rd modular converter 9 network signal being converted to rs 232 serial interface signal, rs 232 serial interface signal is transferred to the 4th modular converter 10 by described 3rd modular converter 9, described 4th modular converter 10 converts the rs 232 serial interface signal of reception to control signal and is transferred to data transmission module 11, described data transmission module 11 pairs of unmanned planes 1 control, described control terminal 2 comprises the operating grip 6 providing control signal to the first modular converter 7, the control signal received is converted to rs 232 serial interface signal and is transferred to the second modular converter 8 by described first modular converter 7, rs 232 serial interface signal is converted to network signal and carries out Signal transmissions communication by Ethernet and the 3rd modular converter 9 by described second modular converter 8, described control terminal 2 comprises arm processor and 16 figure place weighted-voltage D/A converters, data delay≤the 200ms of described control terminal 2, total power consumption≤10W, packet loss≤0.5 ‰.
Embodiment 2
As shown in Figure 2, the present embodiment improves on the basis of embodiment 1, and other structures are identical, and difference is; Described control terminal 2 also comprises the flight course planning display screen 4 that carries out Signal transmissions with operating grip 6 each other and The Cloud Terrace takes display screen 5.
The present invention is not limited to above-mentioned embodiment, and when not deviating from flesh and blood of the present invention, any distortion that it may occur to persons skilled in the art that, improvement, replacement all fall into protection scope of the present invention.

Claims (5)

1. a unmanned plane tele-control system, it is characterized in that, described system comprises the electronic equipment (3) controlled unmanned plane (1) by wireless signal, described electronic equipment (3) carries out network signal transmission by Ethernet and control terminal (2), described electronic equipment (3) comprises the 3rd modular converter (9) network signal being converted to rs 232 serial interface signal, rs 232 serial interface signal is transferred to the 4th modular converter (10) by described 3rd modular converter (9), the rs 232 serial interface signal of reception is converted to control signal and is transferred to data transmission module (11) by described 4th modular converter (10), described data transmission module (11) controls unmanned plane (1).
2. unmanned plane tele-control system according to claim 1, it is characterized in that, described control terminal (2) comprises the operating grip (6) providing control signal to the first modular converter (7), the control signal received is converted to rs 232 serial interface signal and is transferred to the second modular converter (8) by described first modular converter (7), and rs 232 serial interface signal is converted to network signal and carries out Signal transmissions communication by Ethernet and the 3rd modular converter (9) by described second modular converter (8).
3. unmanned plane tele-control system according to claim 2, it is characterized in that, described control terminal (2) comprises the flight course planning display screen (4) that carries out Signal transmissions with operating grip (6) each other and The Cloud Terrace takes display screen (5).
4. unmanned plane tele-control system according to claim 1, it is characterized in that, described control terminal (2) comprises arm processor and 16 figure place weighted-voltage D/A converters.
5. unmanned plane tele-control system according to claim 1, is characterized in that, the data delay≤200ms of described control terminal (2), total power consumption≤10W, packet loss≤0.5 ‰.
CN201610070942.6A 2016-02-02 2016-02-02 Unmanned aerial vehicle remote control system Pending CN105527954A (en)

Priority Applications (1)

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Application Number Priority Date Filing Date Title
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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107256033A (en) * 2017-07-10 2017-10-17 重庆大学 A kind of no-manned machine distant control chromacoder
CN109004972A (en) * 2018-07-13 2018-12-14 深圳市道通智能航空技术有限公司 Data transmission method, device, system and the surface map transmission module of UAV system

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CN103051373A (en) * 2012-12-24 2013-04-17 北京航天科工世纪卫星科技有限公司 Self-rotor unmanned aerial vehicle-based air emergency communication system
CN203504763U (en) * 2013-09-29 2014-03-26 常州中飞航空技术有限公司 Wireless communication device suitable for ground monitoring of pesticide spraying unmanned aerial vehicle
CN204316545U (en) * 2015-01-13 2015-05-06 东莞极飞无人机科技有限公司 Based on the Unmanned Aerial Vehicle Data link system of mobile communications network
CN104802986A (en) * 2015-05-06 2015-07-29 山东师范大学 Emergency medical aid UAS (Unmanned Aircraft System) based on 3G/4G network
CN204669524U (en) * 2015-04-21 2015-09-23 广州迈天智能科技有限公司 A kind of unmanned plane control system based on mobile Internet
CN204761600U (en) * 2015-06-30 2015-11-11 江苏首控制造技术有限公司 Live monitored control system of handheld terminal remote of unmanned aerial vehicle
CN204925801U (en) * 2015-09-09 2015-12-30 深圳市浩瀚卓越科技有限公司 Changeable communication mode's unmanned aerial vehicle control system

Patent Citations (7)

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Publication number Priority date Publication date Assignee Title
CN103051373A (en) * 2012-12-24 2013-04-17 北京航天科工世纪卫星科技有限公司 Self-rotor unmanned aerial vehicle-based air emergency communication system
CN203504763U (en) * 2013-09-29 2014-03-26 常州中飞航空技术有限公司 Wireless communication device suitable for ground monitoring of pesticide spraying unmanned aerial vehicle
CN204316545U (en) * 2015-01-13 2015-05-06 东莞极飞无人机科技有限公司 Based on the Unmanned Aerial Vehicle Data link system of mobile communications network
CN204669524U (en) * 2015-04-21 2015-09-23 广州迈天智能科技有限公司 A kind of unmanned plane control system based on mobile Internet
CN104802986A (en) * 2015-05-06 2015-07-29 山东师范大学 Emergency medical aid UAS (Unmanned Aircraft System) based on 3G/4G network
CN204761600U (en) * 2015-06-30 2015-11-11 江苏首控制造技术有限公司 Live monitored control system of handheld terminal remote of unmanned aerial vehicle
CN204925801U (en) * 2015-09-09 2015-12-30 深圳市浩瀚卓越科技有限公司 Changeable communication mode's unmanned aerial vehicle control system

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107256033A (en) * 2017-07-10 2017-10-17 重庆大学 A kind of no-manned machine distant control chromacoder
CN107256033B (en) * 2017-07-10 2020-12-22 重庆大学 Unmanned aerial vehicle remote control signal conversion equipment
CN109004972A (en) * 2018-07-13 2018-12-14 深圳市道通智能航空技术有限公司 Data transmission method, device, system and the surface map transmission module of UAV system
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CN109004972B (en) * 2018-07-13 2020-09-15 深圳市道通智能航空技术有限公司 Data transmission method, device and system of unmanned aerial vehicle system and ground map transmission module
US11792129B2 (en) 2018-07-13 2023-10-17 Autel Robotics Co., Ltd. Data transmission method, device and system of unmanned aerial vehicle system and ground image transmission module

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Inventor after: Guo Qihong

Inventor after: Li Chao

Inventor after: Wang Lianhui

Inventor after: Zhang Lijiao

Inventor after: Sun Yang

Inventor before: Guo Qihong

Inventor before: Sun Yang

Inventor before: Zhang Pei

Inventor before: Yang Yongqiang

Inventor before: Li Chao

Inventor before: Lin Kang

Inventor before: Zhou Quan

Inventor before: Zu Jinge

Inventor before: Wang Lianhui

Inventor before: Zhang Lijiao

COR Change of bibliographic data
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20160427