Robust missile autopilot design via high-order sliding mode control
Author:
Affiliation:
1. Alabama, Univ., Huntsville
2. U.S. Army, Space and Missile Defense Command, Huntsville, AL
3. Schafer Corp., Huntsville, AL
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3968
Reference20 articles.
1. Guidance and Control of Aerospace Vehicles, C.T. LeondesEd.,McGraw-Hill,N.Y., 1963.
2. Tailoring theory to practice in tactical missile control
3. Agile Missile Dynamics and Control
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