Control system and method for unmanned helicopter with combined guided weapons

A technology of unmanned helicopters and control systems, which is applied in the field of unmanned helicopter control systems, and can solve the problems of unmanned helicopters not disclosed

Active Publication Date: 2018-04-06
BEIJING INSTITUTE OF TECHNOLOGYGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the prior art does not disclose an unmanned helicopter that can mount weapons and monitor and fight.

Method used

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  • Control system and method for unmanned helicopter with combined guided weapons
  • Control system and method for unmanned helicopter with combined guided weapons
  • Control system and method for unmanned helicopter with combined guided weapons

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Experimental program
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Effect test

Embodiment approach

[0100] According to a preferred embodiment of the present invention, the step 1 includes the following sub-steps:

[0101] Step 1-1, use the aiming device 12 to search for the target, and transmit the image information detected during the search to the manipulating seat 22 for stabilizing the aiming;

[0102] Wherein, the image information detected by the aiming device 12 is directly transmitted to the airborne data link terminal 11; and the aiming control seat 22 transmits the received image information to the weapon control seat 24 in real time;

[0103] Step 1-2, the aiming control seat 22 controls the aiming device 12 to detect, identify and lock the target according to the image information transmitted by the aiming device 12;

[0104] Step 1-3, after the aiming device 12 locks the target, the aiming device 12 tracks and locates the target under the control of the aiming control seat 22, and then optionally, the aiming device 12 emits a laser to the target;

[0105] Wher...

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Abstract

The invention discloses a control system and method for an unmanned helicopter with combined guided weapons. The system comprises a helicopter-mounted sub system and a ground sub system, the helicopter-mounted sub system comprises a weapon module, and the image guided weapon and the laser guided weapon are loaded in the weapon module and comprise an image guiding head and a laser guiding head correspondingly. The method comprises the following steps that 1, a target is searched, detected, recognized, locked, traced and positioned, and optionally, a stably-aiming device emits a laser to the target; 2, a flying area is adjusted to enable the target to be within the searching rage of the image guiding head and/or enable the laser guiding head to receive the laser diffused by the target; 3, apowering-on instruction is sent out by a weapon manipulating part to control the image guiding head and/or the laser guiding head to be powered on; and 4, an ignition instruction is sent out by the weapon manipulating part to conduct launching of the image guided weapon and/or the laser guided weapon, and thus target attacking is achieved.

Description

technical field [0001] The present invention relates to an unmanned helicopter, in particular to an unmanned helicopter with hybrid guidance, in particular to a control system and a control method for the unmanned helicopter with hybrid guidance. Background technique [0002] In modern warfare, attacking some fleeting maneuvering targets and time-sensitive targets is the key to combat. In the prior art, most of the fixed-wing aircraft that can carry weapons and carry out strikes are fixed-wing aircraft, but fixed-wing aircraft cannot hover to illuminate, cannot hover to attack, and have the disadvantages of carrying heavy weights. [0003] For the above-mentioned defects, the use of unmanned helicopters can be effectively solved, because unmanned helicopters can achieve hovering irradiation and hovering attacks, and, compared with manned helicopters, unmanned helicopters are unmanned, have high personal safety, and are small in size. Small, difficult to be detected, simple ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41G9/00G05D1/12
CPCF41G9/00G05D1/12
Inventor 林德福朱永伟王江宋韬王伟王辉唐攀余婉铭林时尧叶剑川
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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