Attitude control of missiles via finite-terms Fliess expansion

Authors:
Yupeng Qiao;Dongbin Shen
Affiliations:
College of Automation Science and Engineering, South China University of Technology, Guangzhou, China;College of Automation Science and Engineering, South China University of Technology, Guangzhou, China
Venue:
CCDC'09 Proceedings of the 21st annual international conference on Chinese Control and Decision Conference
Year:
2009

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Nonlinear Control Systems

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Non-regular feedback linearization of nonlinear systems via a normal form algorithm

Automatica (Journal of IFAC)

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Abstract

This paper investigates the attitude control of missiles. We use the decomposed Fliess functional expansion of input-output decomposable systems to describe the outputs. Then under piece-wise constant admissible value controls, the optimal control on finite time durations can be obtained. The method tremendously reduces the complexity of computation and makes the online control design available. The effectiveness of the proposed method is shown by numerical simulations.