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Missile autopilot design via a modified LPV synthesis technique

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Keywords: LMI techniques; Linear Parameter-Varying Control; commande LPV; commande robuste; robust control; techniques LMI

Document Type: Research Article

DOI: http://dx.doi.org/10.1016/S1270-9638(99)80039-X

Affiliations: ONERA-DCT/DCSD, Systems Control and Flight Dynamics Department, BP 4025, 31055 Toulouse cedex 04, France

Publication date: April 1, 1999

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