Taking the attitude control system of micro quad-rotor as a research object, a design scheme of fault estimator based on generalized Kalman-Yakubovic-Popov(GKYP
The reentry trajectory planning for hypersonic vehicles is critical and challenging in the presence of numerous nonlinear equations of motion and path constrain
This study concentrates on management problems of the new generation of the agile earth observation satellite(AEOS). AEOS is a key study object in many countrie