Nonlinear Optimal Control Design of a Missile Autopilot
Conference, Guidance, navigation and control ; 1998 ; Boston; MA
01.01.1998
8 pages
See also same s/m for separate paper nos 4238 to 4494 with gaps held only
Aufsatz (Konferenz)
Englisch
guidance , navigation , control , AIAA
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Nonlinear optimal control design of a missile autopilot
AIAA | 1998
|Missile Autopilot Design Using Nonlinear H~ Optimal Control
British Library Conference Proceedings | 1995
|Robust Nonlinear Missile Autopilot Design
British Library Conference Proceedings | 1995
|Software tools for nonlinear missile autopilot design
AIAA | 1999
|