Autopilot Design for the Advanced Kinetic Energy Missile (ADKEM) Boost Phase
Guidance, navigation and control conference ; 1993 ; Monterey; CA
1993-01-01
11 pages
In 3 vols
Conference paper
English
AIAA , guidance , navigation , control
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Feedback Linearization Autopilot Design for the Advanced Kinetic Energy Missile Boost Phase
Online Contents | 1995
|Missile Autopilot Design During Boost Phase Using Robust Backstepping Approach (AIAA 2015-0860)
British Library Conference Proceedings | 2015
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