Adaptive, Integrated Guidance and Control for Missile Interceptors
Author:
Affiliation:
1. Barron Associates Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-4880
Reference26 articles.
1. Integrated missile guidance and control: a state dependent Riccati differential equation approach
2. Integrated Guidance-Control Systems for Fixed-Aim Warhead Missiles
3. Optimal Fixed-Interval Integrated Guidance-Control Laws for Hit-to-Kill Missiles
4. Invertibility and trajectory control for nonlinear maneuvers of aircraft
5. A dynamic inversion based control law with application to the high angle-of-attack research vehicle
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