AIAA-2002-4658 Improving Transient Performance of Dynamic Inversion Missile Autopilot by Use of Backstepping
Conference, Guidance, navigation and control ; 2002 ; Monterey, CA
2002-01-01
9 pages
Aufsatz (Konferenz)
Englisch
AIAA , guidance , navigation , control
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Missile Autopilot Design During Boost Phase Using Robust Backstepping Approach (AIAA 2015-0860)
British Library Conference Proceedings | 2015
|AUTOPILOT DESIGN FOR AN AGILE MISSILE USING L1 ADAPTIVE BACKSTEPPING CONTROL
British Library Conference Proceedings | 2012
|