Anti-disturbance method for UAV-borne missile launch
A missile launching and anti-disturbance technology, which is applied in the direction of launching devices, weapon accessories, offensive equipment, etc., to solve the disturbance problem, ensure the safety of the aircraft, and the safety of the separation of the aircraft and bombs
Active Publication Date: 2014-02-26
CHINA ACAD OF AEROSPACE AERODYNAMICS
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Problems solved by technology
At present, the launch technology of man-machine missiles is very mature, and the launch of unmanned aerial vehicles is still in its infancy. In this regard, foreign countries only have successful application experience in a very small number of unmanned aerial vehicles such as the Predator, and there is no precedent in China.
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The invention relates to an anti-disturbance technology for unmanned aerial vehicle-borne missile launch, which can solve the disturbance problem of unmanned aerial vehicle-borne missile launch. It is characterized in that it includes the stability and maneuverability design of the carrier aircraft, the layout design of the external store and the design of the launching rack. Through the design of aircraft stability and maneuverability, the aircraft can quickly recover after being disturbed; through the layout design of the external hanger and the design of the launcher, the compatibility problem between the aircraft, the suspension device, and the suspension is comprehensively solved; by selecting a reasonable launch Mode, installation angle and launcher parameters, etc. to reduce the interference of missile launches on UAVs
Description
technical field The invention relates to an anti-disturbance method for launching missiles carried by unmanned aerial vehicles, which can solve the disturbance problem of missiles launched by unmanned aerial vehicles. Background technique The anti-disturbance technology of UAV-borne missile launch can solve the disturbance problem of UAV-borne missile launch. Disturbances in the process of launching missiles by UAVs will cause changes in the attitude of the aircraft on the one hand. If the disturbance is too large, it may threaten the safety of the aircraft or cause the target reconnaissance and indication platform of the aircraft to lose the target. On the other hand, it will cause the attitude of the missile to derail. Unstable, for the aircraft capture and control combat mode, the seeker may lose the target, or affect the hit accuracy. The invention solves the disturbance problem in the process of launching the missile by the UAV by adopting the improvement measures in t...
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IPC IPC(8): F41G9/00F41F7/00
Inventor 曾立科刘凯金延伟
Owner CHINA ACAD OF AEROSPACE AERODYNAMICS