Nonlinear Missile Autopilot Design with Theta-D Technique
Author:
Affiliation:
1. University of Missouri–Rolla, Rolla, Missouri 65409
2. Boeing Company, St. Louis, Missouri 63166
3. Naval Surface Weapon Center, Dahlgren, Virginia 22448-5000
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.1217
Reference24 articles.
1. Modern control theory for design of autopilots for bank-to-turn missiles
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