Coupled LPV and flatness based approach for low lift re-entry vehicule guidance
Automatic Control in Aerospace, Volume # 17 | Part# 1
Authors
Zerar, Madjid; Cazaurang, Franck; Zolghadri, Ali
Digital Object Identifier (DOI)
10.3182/20070625-5-FR-2916.00033
Page Numbers:
189-194
Index Terms
flat systems,path tracking,linear parameter varying systems (LPV),LPV control,re-entry vehicle guidance
Abstract
This paper presents a flatness and LPV-based methodology for an Apollo-Like Re-entry vehicle (ALRV) guidance. The main contribution is considered to be a proposition which converts the original nonlinear longitudinal ALRV flat model into a fictitious Linear Parameter Varying (LPV) model over which a LPV control law can be designed using a finite set of Linear Matrix Inequalities (LMIs). It is shown that the overall scheme is able to ensure robust stability and robust performances when off-nominal conditions are present. Finally, simulation results are presented to demonstrate the potential of the proposed approach.
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