Synthesis of robust feedback missile control strategies by using LMI techniques
conference paper
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.
Topics
Effective toolFeedback strategiesGuidance lawsHorizon control strategyLarge classLMI techniquesMissile controlMissile guidance lawsModel based approachModel uncertaintiesNon-linear dynamicsRobust designsUpper BoundElectronic guidance systemsLinear matrix inequalitiesNavigationUncertainty analysisNonlinear feedback
TNO Identifier
425205
ISBN
9781563479786
Source title
AIAA Guidance, Navigation, and Control Conference and Exhibit, Chicago, IL, USA, 10-13 August 2009 (Conference code: 81960)
Files
To receive the publication files, please send an e-mail request to TNO Repository.