Abstract
Flight vehicle attitude control is of great importance. In this paper, a flight controller based on active disturbance rejection control (ADRC) is proposed. Then stability margin tester is utilized to tune the parameters of the controller to meet the specified stability margins, which will serve as a practical tuning method in practice. Moreover, the CAD software based on MATLAB GUI is designed to integrate the tuning and simulation process. Then the simulations are implemented to demonstrate the effectiveness of this controller and tuning method.
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