Design of Launch Vehicle Flight Control Systems Using Ascent Vehicle Stability Analysis Tool
AIAA Guidance, Navigation, and Control Conference ; 2011 ; Portland, OR
2011-01-01
16 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
Aeroacoustics , CEAS , AIAA
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Hybrid Adaptive Launch Vehicle Ascent Flight Control
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