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Robust stability analysis of a lateral flight control system for a missile

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2 Author(s)
White, B.A. ; Dept. of Aerosp. Power & Sensors, R. Mil. Coll. of Sci., Shrivenham, UK ; Tsourdos, A.

A homing missile lateral autopilot is synthesized by exploiting the fact that under mild differentiability conditions, nonlinear systems can be represented in quasilinear form. The robustness of the lateral missile velocity autopilot to uncertain aerodynamic parameters is then determined using Kharitonov's theorem

Published in:

American Control Conference, 1999. Proceedings of the 1999  (Volume:6 )

Date of Conference:

1999

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