Design of helicopter stabilization systems using optimal control theory.
Author:
Affiliation:
1. Sikorsky Aircraft, Division of United Aircraft Corporation, Stratford, Conn.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44019
Reference6 articles.
1. Synthesis of feedback controls using optimization theory--An example
2. Adaptive Control Processes
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