Optimal Linear-Quadratic Missile Guidance Laws with Penalty on Command Variability
Author:
Affiliation:
1. Department of Aerospace Engineering, TNO Organization, 2280 AA Rijswijk, The Netherlands
2. Faculty of Aerospace Engineering, Department of Aerospace Engineering, Technion—Israel Institute of Technology, 32000 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/10.2514/1.G000738
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