CN109808907A - Autonomous the boat technology of pilotless helicopter - Google Patents
Autonomous the boat technology of pilotless helicopter Download PDFInfo
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- CN109808907A CN109808907A CN201711177663.0A CN201711177663A CN109808907A CN 109808907 A CN109808907 A CN 109808907A CN 201711177663 A CN201711177663 A CN 201711177663A CN 109808907 A CN109808907 A CN 109808907A
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- unmanned helicopter
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- carrier
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Abstract
Unmanned helicopter is a kind of by wireless remotecontrol or by airborne computer program autonomous control aviation aircraft;Relatively fixed wing aircraft, it takes off, land all should not runway, fly more flexible, therefore with stronger survival ability;Compared with manned aircraft, its cab space for not needing pilot first, so unmanned helicopter is small in size, in contrast cost is lower;Secondly, the unpiloted characteristic of unmanned helicopter so that its use is not required to consider the safety problem and fatigue factor of pilot, thus operational environment is required it is low, use it is also more convenient, can be for completing the impossible task of manned aircraft;Most of all, unmanned helicopter is widely used, such as: at civilian aspect, unmanned helicopter can be used for power-line patrolling and stringing, the detection of geology the condition of a disaster, traffic monitoring, resources observation, ground mapping, forest fire protection is sprayed insecticide, and weather information is collected, maritime affairs search, meagrely-populated territory, marine monitoring etc.;At military aspect, unmanned helicopter can be used for going on patrol, target drone, reconnaissance and surveillance, deceive enemy's bait, and electronic countermeasure implements interference, and air-to-ground attack is antisubmarine, and school is penetrated, early warning, communication relay, and transport is anti-ballistic etc..
Description
Technical field
It is an important basic function of carrier-borne unmanned helicopter that the present invention, which is with autonomous landing on the ship,;Due to middle-size and small-size
Tail wind is extremely complex when limited space and the Ship Motion of landing on naval vessel, and aircraft fall ratio on middle-size and small-size naval vessel exists
Land on land or aircraft carrier much dangerous;Therefore, a set of high-precision guidance system is designed to assist unmanned helicopter
Warship have very important researching value;The one kind of guidance system based on computer vision as guide mode, with other
Guide mode is compared, it has many advantages, such as, and at low cost, precision is high, strong antijamming capability.
Background technique
With the continuous variation of marine battlefield means of warfare, Shipborne UAV will become modern surface ship combat system
Essential component part;But there is also many skills at present for development, equipment and the deployment of carrier-borne unmanned helicopter
Art problem, wherein a more crucial technology be unmanned helicopter warship safety issue;Warship safety issue
Threat mainly from two aspects: first is that sea meteorological condition is complicated, fallen when naval vessels are with from when wave and with control, front and back
It waves;Second is that structure is complicated for Ship Air tail flow field, coverage is big, and helicopter rotor blade flexible elongated, rotor scan
Area is big, more sensitive to outer gas stream variation, and the uneven distribution characteristic of Ship air wake will lead to helicopter preshoot entrance
Vortex region is prone to accidents.
Summary of the invention
Solution of the invention is first close to rear the characteristics of landing when being landed according to unmanned helicopter, by nobody
The guiding of driving helicopter is divided into two stages of guiding when close guiding and landing, has determined to the different guiding stages
Different guide modes;The coordinate system and its transformation relation that computer vision guiding needs to use are had studied, a knowledge is devised
Not quickly, the auxiliary landing mark of guidance information can also be provided when being unable to perfect imaging;Close to guiding stage, research
The recognizer of auxiliary landing mark and the extraction of track algorithm and guidance information;To the auxiliary landing mark taken
It is that image is tested the result shows that: auxiliary landing mark is readily identified, track algorithm to auxiliary landing mark track stablize, energy
Effectively extract guidance information.
Specific embodiment
Present invention implementation is as follows, in the landing guiding stage, has studied change in location rule of the warship point by Lidar Equation, with
And thus mark caused by change in location and aircraft position reduce can only partially be imaged or even part edge imaging;For auxiliary
The case where character portion that lands is imaged the characteristics of composition according to auxiliary landing sign body annulus, proposes one by portion
Center location and image center location relationship that the estimation of cyclotomy arc is got determine the class 4 quadrant detector of guidance information;To part
The auxiliary landing mark of imaging center location estimation experiment shows: herein for actual conditions center of circle extraction algorithm have compared with
Strong robustness can effectively extract guidance information.
Claims (1)
1. the present invention as sea base aviation strength reasonable supplement carrier-borne unmanned helicopter relative to fixed-wing nobody
Machine, using with unrivaled superiority on the limited naval vessels in space;Firstly, unmanned helicopter is generated by rotor
Lift and propulsive force, can VTOL, can to front, rear, left and right all directions maneuvering flight, can hovering, also have
Good low-speed characteristics, and it is of less demanding to recycling place when recycling, fly relative to the fixed-wing for needing runway to take off
Machine, more saving space.Among other benefits, carrier-borne unmanned helicopter can also execute, and Real-time Battlefield assessment and is swept at mine-laying
Thunder, targeted surveillance positioning, anti-ship and convoy, naval gunfire guidance and correction, electronic countermeasure and communication relay, lock onto target carry out
Strike executes combat duty under core biochemistry or other specific conditions instead of personnel, even carries out the operations such as suicide attacks times
Business.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201711177663.0A CN109808907A (en) | 2017-11-22 | 2017-11-22 | Autonomous the boat technology of pilotless helicopter |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201711177663.0A CN109808907A (en) | 2017-11-22 | 2017-11-22 | Autonomous the boat technology of pilotless helicopter |
Publications (1)
Publication Number | Publication Date |
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CN109808907A true CN109808907A (en) | 2019-05-28 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201711177663.0A Pending CN109808907A (en) | 2017-11-22 | 2017-11-22 | Autonomous the boat technology of pilotless helicopter |
Country Status (1)
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CN (1) | CN109808907A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112258361A (en) * | 2020-08-20 | 2021-01-22 | 南京中智腾飞航空科技研究院有限公司 | Unmanned aerial vehicle intelligence real-time command management system |
CN112258361B (en) * | 2020-08-20 | 2024-05-14 | 南京中智腾飞航空科技研究院有限公司 | Unmanned aerial vehicle intelligent real-time command management system |
-
2017
- 2017-11-22 CN CN201711177663.0A patent/CN109808907A/en active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112258361A (en) * | 2020-08-20 | 2021-01-22 | 南京中智腾飞航空科技研究院有限公司 | Unmanned aerial vehicle intelligence real-time command management system |
CN112258361B (en) * | 2020-08-20 | 2024-05-14 | 南京中智腾飞航空科技研究院有限公司 | Unmanned aerial vehicle intelligent real-time command management system |
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Addressee: Feng Jing Document name: Notification of Publication of the Application for Invention |
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Addressee: Feng Jing Document name: Notice of expiration of the time limit for the trial |
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Application publication date: 20190528 |