A very severe nonlinear is presented because flight parameters vary along with the flight condition in the flight of missile which brings much difficulty to the design of control system.
导弹在飞行过程中,其飞行参数随着飞行条件的变化而发生较大变化,呈现严重的非线性,给控制系统的设计带来较大困难。
The key problem is that the decoupling method and the harmonious control should be studied in the missile flight simulator system control.
所以,在大系统控制中,首要问题是研究解耦方法和协调控制。
The method for consistency check of multisensor data by using the probability distance measuring is presented, and it used in CAN bus missile guidance and control system based on multi-IMU.
提出了应用概率距离测量对多传感器信息进行一致性检验的方法,并将此方法引入到基于多惯性测量组合的总线式导弹制导控制系统中。
应用推荐