In order to solve the problem that the ripple-effect analysis for the operational architecture of air defense systems(OAADS)is hardly described in quantity with
The approach to the synthesis of autopilot with aerodynamic uncertainty is investigated in order to achieve large maneuverability of agile missiles. The dynamic
Traditional orthogonal strapdown inertial navigation system(SINS) cannot achieve satisfactory selfalignment accuracy in the stationary base: taking more than 5