Optimal Flight Control with Nonlinear Actuator Compensation through Model Reference Adaptive Control
AIAA guidance, navigation, and control conference ; 2012 ; Minneapolis, MN
01.01.2012
12 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
Guidance , Control , AIAA , Navigation
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Nonlinear dynamic inversion control with adaptive compensation for flight control system
British Library Online Contents | 1997
|