Fixed-trim re-entry guidance analysis
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia
2. Virginia Polytechnic Institute and State University, Blacksburg, Virginia
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/10.2514/3.19789
Reference10 articles.
1. Merging conventional and optimal control techniques for practical missile terminal guidance
2. 3D'Azzo, J.J. and Houpis, C.H., Feedback Control System Analysis and Sythesis, McGraw-Hill, New York, 1966. pp.529-530.
3. Linear Servo Theory
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