Nonlinear robust missile autopilot design using successive Galerkin approximation
Guidance, Navigation, and Control Conference and Exhibit ; 1999 ; Portland , OR , U.S.A.
01.01.1999
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Nonlinear Robust Missile Autopilot Design Using Successive Galerkin Approximation
British Library Conference Proceedings | 1999
|Robust Nonlinear Missile Autopilot Design
British Library Conference Proceedings | 1995
|Missile autopilot design using robust eigenvalue assignment
TIBKAT | 1992
|Robust Nonlinear Design of a High Incidence Missile Autopilot
British Library Conference Proceedings | 2001
|