Guidance Law Design for Missiles with Reduced Seeker Field-of-View
Author:
Affiliation:
1. Mississippi State University
2. University of Missouri-Rolla
3. Naval Surface Weapon Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-6085
Reference4 articles.
1. A new method for suboptimal control of a class of non-linear systems
2. Bryson,Jr.,A.E.andHo,Y-C.,AppliedOptimalControl,HemispherePublishingCorporation,1975.
3. Nonlinear Missile Autopilot Design with Theta-D Technique
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