This paper studies the flight control problem of hypersonic vehicle considering parameter uncertainties and external disturbances. Firstly, the feedback linearization method is involved to obtain the model of hypersonic vehicle in linear form with mismatched disturbances. On this basis, the nominal controller is used to estimate the compound disturbances and compensate in the controller. Moreover, the design procedure of the state feedback matrix and disturbance compensate matrix is given to stabilize the closed-loop system. The relevancy of the state feedback matrix and disturbance compensate matrix simplify the design process of the controller. In the end, compared simulations are conducted to verify the high performance of the proposed controller.
Anti-Disturbance Feedback Linearization Control for Generic Hypersonic Vehicles
Lect. Notes Electrical Eng.
2021-10-30
16 pages
Article/Chapter (Book)
Electronic Resource
English
Anti-Disturbance Feedback Linearization Control for Generic Hypersonic Vehicles
British Library Conference Proceedings | 2022
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