The invention discloses a satellite-guided defense penetration aircraft and a time constraint guidance control method thereof.The system is internally provided with a satellite navigation module used for obtaining position information and speed information of the aircraft in real time, an IMU module used for obtaining attitude information and acceleration information of the aircraft in real time, and a timing module used for timing the position information and the speed information of the aircraft in real time. The time recording module is used for recording the elapsed time of the aircraft in the flight process after the aircraft takes off in real time, and the microprocessor is used for obtaining a guidance instruction according to the received information; the control module is used for generating a rudder instruction according to the guidance instruction and further controlling the servo steering engine to deflect; wherein in the microprocessor, guidance control is carried out based on an expected flight time error and a flight time error, and required overload is obtained, so that each aircraft can hit a target according to preset time.
本发明公开了一种卫星制导突防飞行器及其上的时间约束制导控制方法,该系统中设置有卫星导航模块,其用于实时获得飞行器的位置信息、速度信息,IMU模块,其用于实时获得飞行器的姿态信息和加速度信息,计时模块,其实时记录飞行器在起飞后的飞行过程中已经经过的时间,微处理器,其用于根据接收到的信息获得制导指令;控制模块,其用于根据制导指令生成舵指令,进而控制伺服舵机偏转;其中,在所述微处理器中,基于期望飞时和飞行时间误差进行制导控制,获得需用过载,从而使得每个飞行器都能够按照预设时间命中目标。
Satellite-guided defense penetration aircraft and time-constrained guidance control method on satellite-guided defense penetration aircraft
卫星制导突防飞行器及其上的时间约束制导控制方法
2024-01-09
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Defense analysis and aircraft penetration mission planning
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