Feedback Linearization Autopilot Design for the Advanced Kinetic Energy Missile Boost Phase
1995
Aufsatz (Zeitschrift)
Unbekannt
Missile Autopilot Design During Boost Phase Using Robust Backstepping Approach (AIAA 2015-0860)
British Library Conference Proceedings | 2015
|Linearization of a Six-Degree-of-Freedom Missile for Autopilot Analysis
Online Contents | 1998
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