Nonlinear Guidance and Navigation of a Tactical Missile with High Heading Error
Author:
Affiliation:
1. Chung Shan Institute of Science and Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-4773
Reference20 articles.
1. Nonlinear Control Systems
2. Guidance of a homing missile via nonlinear geometric control methods
3. Guidance Algorithm Design: A Nonlinear Inverse Approach
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