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[American Institute of Aeronautics and Astronautics AIAA Guidance, Navigation, and Control Conference and Exhibit - Monterey, California ()] AIAA Guidance, Navigation, and Control Conference and Exhibit - A New Optimal Nonlinear Control Method and its Application to Missile Guidance Law Design

✍ Scribed by Xin, Ming; Balakrishnan, S

Book ID: 121051084
Publisher: American Institute of Aeronautics and Astronautics
Year: 2002
Weight: 643 KB
Category: Article
ISBN: 1624101089
DOI: 10.2514/6.2002-5023

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