Lyapunov-Based Nonlinear Missile Guidance
Author:
Affiliation:
1. Universite du Quebec a Trois-Rivieres, Trois-Rivieres, Quebec G9A 5H7, Canada
2. Defence Research and Development Canada–Valcartier, Val-Belair, Quebec G3J 1X5, Canada
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/10.2514/1.8629
Reference16 articles.
1. 1Zarchan, P., Tactical and Strategic Missile Guidance, Vol.199, Progress in Astronautics and Aeronautics, AIAA, Reston,VA, 2002, pp.11-29.
2. Optimal intercept guidance for short-range tactical missiles
3. Optimal guidance for high-order and acceleration constrained missile
4. On Optimal Guidance for Homing Missiles
5. Geometric Approach to Three-Dimensional Missile Guidance Problem
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