Synthesis of flight control and guidance law by output feedback design applied to the interception problem

Abstract

Communication to : 6th ONERA-DLR aerospace symposium, Berlin (Allemagne), 22-23 juin 2004SIGLEAvailable from INIST (FR), Document Supply Service, under shelf-number : 22419, issue : a.2004 n.101 / INIST-CNRS - Institut de l'Information Scientifique et TechniqueFRFranc

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