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- W2761897957 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." @default.
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- W2761897957 date "2017-05-01" @default.
- W2761897957 modified "2023-09-26" @default.
- W2761897957 title "Interactive ADRC design for flight attitude control" @default.
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- W2761897957 doi "https://doi.org/10.1109/ddcls.2017.8068142" @default.
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