All-aspect acceleration-limited homing guidance
Author:
Affiliation:
1. USAF, Research Lab., Eglin AFB, FL
2. Ques Tech, Inc., Niceville, FL
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-4063
Reference12 articles.
1. Agile missile dynamics and control
2. Differential game based guidance law for high angle of attack missiles
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4. A VSS guidance law for agile missiles
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