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Missile Guidance Law Based on Extended State Observer

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4 Author(s)
Zhu, Z. ; Z. Zhu is with the Beijing Institute of Specialized Machinery, Beijing 100143, China. (email: zhuzheng20601521@gmail.com) ; Xu, D. ; Liu, J. ; Xia, Y.

The problem of missile interception is investigated in this paper. Sliding mode controllers with finite time convergence are proposed for the design of guidance laws. Specially, the control design consists of the estimation of the target acceleration by extended state observer (ESO) and thus it achieves the decrease of undesired chattering effectively. Also, simulation results are presented to illustrate the effectiveness of the control strategies.

Published in:
Industrial Electronics, IEEE Transactions on  (Volume:PP ,  Issue: 99 )

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