CN108508907A - Smooth trajectory control system when unmanned plane formation formation converts - Google Patents

Smooth trajectory control system when unmanned plane formation formation converts Download PDF

Info

Publication number
CN108508907A
CN108508907A CN201810101481.3A CN201810101481A CN108508907A CN 108508907 A CN108508907 A CN 108508907A CN 201810101481 A CN201810101481 A CN 201810101481A CN 108508907 A CN108508907 A CN 108508907A
Authority
CN
China
Prior art keywords
unmanned plane
formation
module
controller
point information
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
CN201810101481.3A
Other languages
Chinese (zh)
Inventor
闵锐
邓江华
周荣鑫
覃海群
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.)
Shenzhen Desert Intelligence Control Technology Co Ltd
Original Assignee
Shenzhen Desert Intelligence Control 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 Shenzhen Desert Intelligence Control Technology Co Ltd filed Critical Shenzhen Desert Intelligence Control Technology Co Ltd
Publication of CN108508907A publication Critical patent/CN108508907A/en
Pending legal-status Critical Current

Links

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
    • G05D1/104Simultaneous control of position or course in three dimensions specially adapted for aircraft involving a plurality of aircrafts, e.g. formation flying

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

A kind of smooth trajectory control system when being converted the present invention provides unmanned plane formation formation, including earth station controller, unmanned plane are formed into columns, and the earth station controller is connect with the unmanned plane formation wireless signal, the beneficial effects of the present invention are:The method for realizing smooth trajectory is simpler;It is received in unmanned plane more efficient on way point information;Working efficiency higher.

Description

Smooth trajectory control system when unmanned plane formation formation converts
【Technical field】
A kind of a kind of track when being converted the present invention relates to air vehicle technique field more particularly to unmanned plane formation formation is flat Sliding control system.
【Background technology】
In recent years, the development of unmanned plane was paid attention to by many countries.By development for many years, nowadays unmanned plane has been There are 300 Multiple Types.Miniaturization, intelligence, clustering, digitlization are the developing direction of the following unmanned plane.
In modern war, operational environment becomes increasingly complex, and fighting range is more and more wider, and combat duty tends to diversification, Various air defense technologies are increasingly perfect so that completing task by single unmanned plane becomes hardly possible.It is formed into columns using unmanned plane Execution task can not only provide the ammunition for destroying target enough, and can be the case where certain unmanned planes are found to destroy Under by remaining unmanned plane formation continue to execute task, substantially increase the possibility of completion task.Therefore, in order to adapt to future Challenge, other than improving the function and effectiveness of single machine, it is also necessary to develop significantly more efficient unmanned plane and form into columns management tissue and control Method processed, it is the key concept of the unmanned plane cooperation task development proposed in recent years that unmanned plane, which is formed into columns, but is formed into columns in unmanned plane In terms of the TRAJECTORY CONTROL of formation transformation, controlled there is no reliable method.
【Invention content】
Unmanned plane is solved present invention aims at solution to form into columns during carrying out formation transformation or the line of flight, by The stall problem occurred is sent in destination;It solves due to the extraneous unpredictable factor such as network, caused destination is carrying out Some aircrafts cannot receive the problem of destination when update;It solves unmanned plane and forms into columns carrying out formation transformation or the line of flight In the process, due between aircraft difference with caused by speed issue unmanned plane form into columns can not be synchronous problem deficiency and provide A kind of novel unmanned plane formation formation transformation when smooth trajectory control system.
The present invention is achieved through the following technical solutions:A kind of smooth trajectory control when unmanned plane formation formation transformation System processed, including earth station controller, unmanned plane are formed into columns, and the earth station controller connects with the unmanned plane formation wireless signal It connects.
Further, the unmanned plane formation includes the nothing that several can be communicated wirelessly with earth station controller respectively It is man-machine.
Further, the unmanned plane includes unmanned plane shell, battery, circuit board, and the battery, circuit board are located at described Unmanned plane enclosure interior is additionally provided with several unmanned plane during flying modules on the unmanned plane shell, and the circuit board includes wireless communication Number receiving module, wireless signal transmitting module, processor, GPS positioning module, obstacle detection module, the wireless signal connect Module, wireless signal transmitting module, GPS positioning module, obstacle detection module is received to connect with the processor signal, it is described Unmanned plane during flying module is connect with the processor signal.
Further, the earth station controller includes controller signals transmitting module, controller signals receiving module, control Device processor processed, the controller signals transmitting module, controller signals receiving module with the controller processor signal Connection, the controller signals receiving module receive that unmanned plane wireless signal transmitting module launches according to GPS positioning mould The unmanned plane location information of block positioning;Every frame unmanned plane during the controller signals transmitting module is formed into columns to unmanned plane sends boat Point information;After the reception of wireless signals module of the unmanned plane receives way point information, way point information is sent at unmanned plane Manage device, the unmanned plane update processor way point information.
Further, the earth station controller updates way point information at regular intervals, and by newer way point information It is sent to unmanned plane by controller signals transmitting module.
Further, the way point information includes the velocity information of location information and the every frame unmanned plane destination flight of control.
It forms into columns in use, preparing unmanned plane, unmanned planes more than 10 framves of preparation is formed into columns, and is carried out on after preflight check Electricity, and connect with earth station;To fly-send to each unmanned plane in forming into columns, and by earth station's dramatization, drama shows The way point information of unmanned plane after writing completion, is sent to each unmanned plane in forming into columns by the aircraft trace that unmanned plane is formed into columns, Each unmanned plane during i.e. unmanned plane is formed into columns flies the route given according to drama;Each unmanned plane receives way point information, and The update of destination is carried out, after earth station sends way point information, each unmanned plane in formation starts to receive destination, still, due to The external world such as network unpredictable factor, for destination when every wheel updates, not all unmanned plane can receive the destination of oneself, Therefore, in practical operation, after excessively taking turns destination update, the destination of all unmanned planes is updated, that is, is ensured every Frame unmanned plane can receive way point information;The speed of each destination is controlled.In flight course, unmanned plane differs Cause property causes the rhythm between unmanned plane inconsistent, therefore, in practical operation, by controlling every frame unmanned plane destination flight Speed makes aircraft synchronize;Judge whether the present state of flight of unmanned plane is consistent.Pass through way point information update, destination speed control After system, judge whether the state of all unmanned planes is consistent using information such as speed, the positions of every frame unmanned plane;If state one It causes, then it represents that each unmanned plane that unmanned plane is formed into columns reaches designated state;If state is inconsistent, back to transmission way point information Step updates one time again, until the state of all unmanned planes reaches unanimously;Complete smooth trajectory control.
The beneficial effects of the present invention are:
(1) realize that the method for smooth trajectory is simpler, compared with previous control system, by transmitting destination letter in advance The simpler reality of method of smooth trajectory when breath, more wheel update destinations, control destination speed make unmanned plane formation formation convert With;
(2) more efficient on unmanned plane reception way point information, when each unmanned plane formed into columns to unmanned plane transmits destination, Using taking turns newer mode, it is ensured that every frame unmanned plane can receive the way point information of earth station's transmission, compare conventional method more It is more efficient;
(3) whether working efficiency higher after update and the speed control of completing all destinations, then carries out drone status Consistent judgement indicates that unmanned plane reaches designated state if consistent, completes smooth trajectory control.
【Description of the drawings】
Fig. 1 is smooth trajectory control system architecture schematic diagram when unmanned plane formation formation of the present invention converts;
Fig. 2 is unmanned plane structural schematic diagram of the present invention;
Fig. 3 is earth station controller structural schematic diagram of the present invention;
Fig. 4 is that unmanned plane destination of the present invention update diagram is intended to;
Fig. 5 is the smooth trajectory control system figure that unmanned plane of the present invention is formed into columns when converting formation;
Reference numeral:1, earth station controller;11, controller signals transmitting module;12, controller signals receiving module; 13, controller processor;2, unmanned plane is formed into columns;21, unmanned plane;210, unmanned plane shell;211, battery;212, circuit board; 2120, reception of wireless signals module;2121, wireless signal transmitting module;2122, processor;2123, GPS positioning module; 2124, obstacle detection module;213, unmanned plane during flying module.
【Specific implementation mode】
Below in conjunction with the accompanying drawings and specific implementation mode is described further the present invention:
As shown in figure 1, figure 2, figure 3, figure 4 and figure 5, smooth trajectory control system when a kind of unmanned plane formation formation transformation, Including earth station controller 1, unmanned plane formation 2, the earth station controller 1 is connect with the unmanned plane 2 wireless signals of formation.
Preferably, the unmanned plane formation 2 includes the nothings that several can be communicated wirelessly with earth station controller 1 respectively Man-machine 21.
Preferably, the unmanned plane 21 includes unmanned plane shell 210, battery 211, circuit board 212, the battery 211, electricity Road plate 212 is located inside the unmanned plane shell 210, and several unmanned plane during flying modules are additionally provided on the unmanned plane shell 210, The circuit board 212 includes reception of wireless signals module 2120, wireless signal transmitting module 2121, processor 2122, GPS positioning Module 2123, obstacle detection module 2124, the reception of wireless signals module 2120, wireless signal transmitting module 2121, GPS Locating module 2123, obstacle detection module 2124 are connect with 2122 signal of the processor, the unmanned plane during flying module It is connect with 2122 signal of the processor.
Preferably, the earth station controller 1 includes controller signals transmitting module 11, controller signals receiving module 12, controller processor 13, the controller signals transmitting module 11, controller signals receiving module 12 with the controller 13 signal of processor connects, and the controller signals receiving module 12 receives the transmitting of 21 wireless signal transmitting module 2121 of unmanned plane 21 location information of unmanned plane positioned according to GPS positioning module 2123 to come over;The controller signals transmitting module 11 is to nothing Every frame unmanned plane 21 in man-machine formation 2 sends way point information 3;The reception of wireless signals module 2120 of the unmanned plane 21 receives To after way point information 3, way point information 3 is sent to unmanned plane processor, the unmanned plane update processor way point information 3.
Preferably, the earth station controller 1 updates way point information 3 at regular intervals, and by newer way point information 3 It is sent to unmanned plane 21 by controller signals transmitting module 11.
Preferably, the way point information 3 includes the velocity information of location information and the every frame unmanned plane destination flight of control.
In use, preparing unmanned plane formation 2, unmanned plane formation 2 more than 10 framves of preparation carries out on after preflight check Electricity, and connect with earth station controller 1;To fly-send to each unmanned plane in forming into columns, and be write by earth station controller 1 Drama, drama are the aircraft trace for being demonstrated by unmanned plane formation 2, and after writing completion, the way point information of unmanned plane is sent to Each unmanned plane in each unmanned plane in formation, i.e. unmanned plane formation 2 will fly according to the route that drama gives;It is each nobody Machine receives way point information, and carries out the update of destination, after earth station controller 1 sends way point information, in formation it is each nobody Machine starts to receive destination, and still, due to the extraneous unpredictable factor such as network, destination is when every wheel updates, not all nothing The man-machine destination that can receive oneself, therefore, in practical operation, after excessively taking turns destination update, all unmanned planes Destination is updated, that is, ensures that every frame unmanned plane can receive way point information;The speed of each destination is controlled, In flight course, the inconsistency of unmanned plane causes the rhythm between unmanned plane inconsistent, therefore, in practical operation, leads to The speed for controlling every frame unmanned plane destination flight is crossed, aircraft is made to synchronize;Judge whether the present state of flight of unmanned plane is consistent, leads to It crosses after way point information update, destination speed control, judges all unmanned planes using information such as speed, the positions of every frame unmanned plane State it is whether consistent;If state consistency, then it represents that each unmanned plane that unmanned plane is formed into columns reaches designated state;If state is not Unanimously, then it returns to transmission way point information step to update again one time, until the state of all unmanned planes reaches unanimously;It is complete It is controlled at smooth trajectory.
According to the disclosure and teachings of the above specification, those skilled in the art in the invention can also be to above-mentioned embodiment party Formula carries out change and modification appropriate.Therefore, the invention is not limited in specific implementation modes disclosed and described above, to this Some modifications and changes of invention should also be as falling into the scope of the claims of the present invention.In addition, although this specification In used some specific terms, these terms are merely for convenience of description, does not limit the present invention in any way.

Claims (6)

1. smooth trajectory control system when a kind of unmanned plane formation formation transformation, it is characterised in that:Including earth station controller, Unmanned plane is formed into columns, and the earth station controller is connect with the unmanned plane formation wireless signal.
Smooth trajectory control system when 2. unmanned plane formation formation converts according to claim 1, it is characterised in that:It is described Unmanned plane formation includes the unmanned plane that several can be communicated wirelessly with earth station controller respectively.
Smooth trajectory control system when 3. unmanned plane formation formation converts according to claim 2, it is characterised in that:It is described Unmanned plane includes unmanned plane shell, battery, circuit board, and the battery, circuit board are located at the unmanned plane enclosure interior, the nothing Several unmanned plane during flying modules are additionally provided on man-machine shell, the circuit board includes reception of wireless signals module, wireless signal hair Penetrate module, processor, GPS positioning module, obstacle detection module, the reception of wireless signals module, wireless signal transmission mould Block, GPS positioning module, obstacle detection module are connect with the processor signal, the unmanned plane during flying module with it is described Processor signal connects.
Smooth trajectory control system when 4. unmanned plane formation formation converts according to claim 1, it is characterised in that:It is described Earth station controller includes controller signals transmitting module, controller signals receiving module, controller processor, the controller Signal emission module, controller signals receiving module are connect with the controller processor signal, and the controller signals connect It receives module and receives the unmanned plane position letter positioned according to GPS positioning module that unmanned plane wireless signal transmitting module launches Breath;Every frame unmanned plane during the controller signals transmitting module is formed into columns to unmanned plane sends way point information;The unmanned plane After reception of wireless signals module receives way point information, way point information is sent to unmanned plane processor, the unmanned plane processing Device updates way point information.
Smooth trajectory control system when 5. unmanned plane formation formation converts according to claim 1, it is characterised in that:It is described Earth station controller updates way point information at regular intervals, and newer way point information is passed through controller signals transmitting module It is sent to unmanned plane.
Smooth trajectory control system when 6. unmanned plane formation formation converts according to claim 4, it is characterised in that:It is described Way point information includes the velocity information of location information and the every frame unmanned plane destination flight of control.
CN201810101481.3A 2017-06-21 2018-02-01 Smooth trajectory control system when unmanned plane formation formation converts Pending CN108508907A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN2017207259586 2017-06-21
CN201720725958 2017-06-21

Publications (1)

Publication Number Publication Date
CN108508907A true CN108508907A (en) 2018-09-07

Family

ID=63374856

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810101481.3A Pending CN108508907A (en) 2017-06-21 2018-02-01 Smooth trajectory control system when unmanned plane formation formation converts

Country Status (1)

Country Link
CN (1) CN108508907A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111290430A (en) * 2020-02-17 2020-06-16 一飞智控(天津)科技有限公司 Unmanned aerial vehicle formation dance step uploading transmission control system and method and intelligent terminal
CN112015203A (en) * 2020-09-07 2020-12-01 深圳大漠大智控技术有限公司 Unmanned aerial vehicle cluster trajectory tracking method and system

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007060167A1 (en) * 2005-11-25 2007-05-31 Thales Method for managing a convoy flight
CN104820431A (en) * 2015-05-08 2015-08-05 西北工业大学 Multi-unmanned-aerial-vehicle cluster to-the-ground observation system and formation control method
CN205353654U (en) * 2015-12-09 2016-06-29 广东工业大学 Many aircraft are flight control in coordination
CN205844900U (en) * 2016-07-07 2016-12-28 衢州赋腾信息科技有限公司 A kind of unmanned plane formation control system
CN106843263A (en) * 2016-12-22 2017-06-13 深圳市书呆科技有限公司 Unmanned aerial vehicle flight control method and system
CN206258735U (en) * 2016-12-09 2017-06-16 中国科学院自动化研究所 The aerial demo system of multidimensional based on multiple no-manned plane

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007060167A1 (en) * 2005-11-25 2007-05-31 Thales Method for managing a convoy flight
CN104820431A (en) * 2015-05-08 2015-08-05 西北工业大学 Multi-unmanned-aerial-vehicle cluster to-the-ground observation system and formation control method
CN205353654U (en) * 2015-12-09 2016-06-29 广东工业大学 Many aircraft are flight control in coordination
CN205844900U (en) * 2016-07-07 2016-12-28 衢州赋腾信息科技有限公司 A kind of unmanned plane formation control system
CN206258735U (en) * 2016-12-09 2017-06-16 中国科学院自动化研究所 The aerial demo system of multidimensional based on multiple no-manned plane
CN106843263A (en) * 2016-12-22 2017-06-13 深圳市书呆科技有限公司 Unmanned aerial vehicle flight control method and system

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111290430A (en) * 2020-02-17 2020-06-16 一飞智控(天津)科技有限公司 Unmanned aerial vehicle formation dance step uploading transmission control system and method and intelligent terminal
CN112015203A (en) * 2020-09-07 2020-12-01 深圳大漠大智控技术有限公司 Unmanned aerial vehicle cluster trajectory tracking method and system
CN112015203B (en) * 2020-09-07 2024-04-02 深圳大漠大智控技术有限公司 Unmanned aerial vehicle cluster track tracking method and system

Similar Documents

Publication Publication Date Title
US20200372808A1 (en) Secure unmanned aerial vehicle flight planning
CN105892476B (en) A kind of control method and controlling terminal of aircraft
CN103246204B (en) Multiple no-manned plane system emulation and verification method and device
CN105842717A (en) Anti-UAV(unmanned aerial vehicle) method and system
CN106656300A (en) UAV cluster combat system utilizing ad-hoc network data chain
US20200105150A1 (en) Unmanned aircraft return flight control method, device, and unmanned aerial vehicle
CN103176475A (en) Ground station for unmanned aerial vehicles
CN108759837A (en) Unmanned plane multi computer communication combat system and method
WO2018028358A1 (en) Method, apparatus and system for implementing formation flying
CN108521667B (en) Unmanned aerial vehicle data transmission method with low transmission energy consumption
CN106347694B (en) A kind of Information Acquisition System based near space floating platform
CN107861522A (en) Unmanned target drone control system
CN109398709B (en) External airborne weapon fire control system and use method
CN104303016B (en) Integrated complex of on-board equipment for multifunctional aeroplane
CN107302394A (en) A kind of unmanned aerial vehicle (UAV) control method based on Big Dipper short message
CN105597308A (en) Unmanned plane, simulative air combat gaming device and simulative air combat gaming system
CN104575109B (en) Signal processing method of transmitting link of ADS-B system
CN108508907A (en) Smooth trajectory control system when unmanned plane formation formation converts
CN106483980A (en) A kind of unmanned plane follows the control method of flight, apparatus and system
CN107305395A (en) Unmanned plane method and system
CN107087441B (en) A kind of information processing method and its device
CN110377054B (en) Unmanned aerial vehicle cluster control system and method based on airborne platform
CN109116861A (en) A kind of unmanned aerial vehicle ground control system
CN109398716B (en) External airborne control system
CN114697248B (en) Unmanned aerial vehicle information attack semi-physical test system and 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