Integrated missile guidance law and autopilot design using linear optimal control
Author:
Affiliation:
1. Florida, Univ., Gainesville
2. USAF, Research Lab., Eglin AFB, FL
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-4163
Reference6 articles.
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