Control system and control method for unmanned helicopter with laser guidance weapon

An unmanned helicopter and laser-guided technology, which is applied in the control of finding targets and other directions, can solve the problems of unmanned helicopters that are not disclosed.

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

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Problems solved by technology

[0004] However, the prior art does not disclose an unmanne

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  • Control system and control method for unmanned helicopter with laser guidance weapon
  • Control system and control method for unmanned helicopter with laser guidance weapon
  • Control system and control method for unmanned helicopter with laser guidance weapon

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Embodiment approach

[0083] According to a preferred embodiment of the present invention, the ground subsystem 2 includes a ground data link terminal 21 , a steady sight control seat 22 , a flight control control seat 23 , a weapon control seat 24 and a ground task manager 25 .

[0084] Wherein, the ground data link terminal 21 is used for information transmission with the airborne subsystem 1, and the information includes the data information and image information sent by the airborne subsystem 1 to the ground subsystem 2 and the data information and image information sent by the ground subsystem 2 to the aircraft subsystem. The instruction information of the carrier subsystem 1; the stabilized aiming control seat 22 is used to control the stabilized aiming device 12, so as to realize the search and tracking of the target, and is used for post-war evaluation; the flight control control seat 23 is used to control The flight control module 13 controls the flight of the unmanned helicopter; the weapo...

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Abstract

The invention discloses a control system and control method for an unmanned helicopter with a laser guidance weapon. The system is composed of an onboard subsystem and a ground subsystem. The onboardsubsystem consists of an onboard data link terminal, a stable aiming device, a flight control module, a weapon module, and an on-board task management device; a weapon is carried inside the weapon module; and a laser guidance head including a laser receiver is arranged at the weapon. The ground subsystem includes a ground data link terminal, a stable aiming operation seat, a flight control seats,a weapon control seat and a ground task management device. In addition, the method comprises: step one, target searching, detections, identification, locking, tracking, and positioning are carried outand then the stable aiming device emits laser to the target; step two, a flight zone is adjusted and thus the laser receiver is able to receive laser after diffuse reflection by the target; step three, the weapon control seat sends out a power-on instruction and the laser guidance head is controlled to be electrified; and step four, the weapon control seat sends out an ignition instruction to carry out target striking.

Description

technical field [0001] The present invention relates to an unmanned helicopter, in particular to an unmanned helicopter with laser guidance, in particular to a control system and a control method for the unmanned helicopter with laser 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 st...

Claims

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Application Information

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IPC IPC(8): G05D1/12
CPCG05D1/12
Inventor 王江朱永伟宋韬林德福王伟王辉唐攀余婉铭林时尧叶剑川
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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