Synthesis of robust feedback missile control strategies by using LMI techniques

Synthesis of robust feedback missile control strategies by using LMI techniques

Trottemant, E.J.
Weiss, M.
Vermeulen, A.
TNO Defensie en Veiligheid

2009

Robust programming, and more specific LMI techniques, have proven to be an extremely effective tool for the synthesis of missile guidance laws. The advantage of this model-based approach is that a large class of uncertainties can be taken into account and a robust guidance law is obtained. In this paper the class of uncertainties applicable for robust design is extended to include non-linear dynamics. Hence the obtained robust disturbance feedback strategies provide an upper bound on the performance of the nonlinear system against all allowable evader disturbances and model uncertainties. Furthermore it is shown that implementing the strategies as a receeding horizon control strategy lead to very satisfactory results. Copyright © 2009 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.

Weapon systems
Effective tool
Feedback strategies
Guidance laws
Horizon control strategy
Large class
LMI techniques
Missile control
Missile guidance laws
Model based approach
Model uncertainties
Non-linear dynamics
Robust designs
Upper Bound
Electronic guidance systems
Linear matrix inequalities
Navigation
Uncertainty analysis
Nonlinear feedback

http://resolver.tudelft.nl/uuid:ed62edce-99a1-4aa5-bbe1-8bc3b925e572

425205

AIAA 2009-5642

9781563479786

AIAA Guidance, Navigation, and Control Conference and Exhibit, Chicago, IL, USA, 10-13 August 2009 (Conference code: 81960)

conference paper