Optimal guidance law in the plane
Author:
Affiliation:
1. Laboratoire d'Automatique Theorique, Paris, France
2. Technion, Haifa, Israel
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/10.2514/3.19880
Reference19 articles.
1. Linear feedback solutions for minimum effort interception, rendezvous, and soft landing
2. Optimal intercept guidance for short-range tactical missiles
3. Comparison of Optimal Control and Differential Game Intercept Missile Guidance Laws
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