1.Put the disturbance moments of typical astronaut’s push-off act as the input datas of the control system simulation, and analyze the response of the attitude control system after disturbed.
2.Diagonal matrix, model inverse and incomplete state feedback method were discussed to decouple the attitude, and poles configuration was adopted to improve the control system dynamic response for the last method.
3.Employing the above design method, the decoupling flight control system of UH 60A helicopter is designed for attitude command attitude hold (ACAH) response type. The simulation results show that the validity of the decoupling control design method with too fast mode of controller being limited.
4.The objectives that were set by ESI and MSCAA were aimed at gaining a better understanding the AEP, identifying opportunities for training, achieving a change in attitude in and about the over all emergency response plan for Memphis International Airport.
5.Using kinetic kill vehicle to intercept tactical ballistic missile (TBM) during terminal phase, the advantage of Divert and Attitude Control System (DACS) whose response time is very short is taken to improve accuracy and destroy the target by hit-to-kill technology.
