3Three Dimension Two Phase Flow Field Numerical Simulation on Tail-Pipe Nozzle SRM under Spinning Condition10-15
7Linear Quadratic Optimal Control for Discrete-Time Markov Jump System with Multiplicative and Additive Noise32-36
9Research on Firepower Distribution Model of Surface to Air Missile ased on Differential Evolution Algorithm41-44
12The Fault Diagnosis of the Aircraft Electromechanical Actuation System Based on Wavelet Transformation55-58