Agile missile dynamics and control
Author:
Affiliation:
1. McDonnell Douglas Aerospace, Saint Louis, MO
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-3912
Reference9 articles.
1. Robust hover control for a short takeoff/vertical landing aircraft
2. Comparison of six robustness tests evaluating missile autopilot robustness to uncertain aerodynamics
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