Affiliation:
1. Massachusetts Institute of Technology, Cambridge, Massachusetts 02139
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
Reference29 articles.
1. 2Shaw, J. "A Feasibility Study of Helicopter Vibration Reduction by Self-Optimizing Higher Harmonic Blade Pitch Control," M.S. Thesis,Dept. of Aeronautics and Astronautics, Massachusetts Inst. of Technology, Cambridge, MA,1967.
2. Helicopter Vibration Reduction with Higher Harmonic Blade Pitch
3. A Unified Approach to the Optimal Design of Adaptive and Gain Scheduled Controllers to Achieve Minimum Helicopter Rotor Vibration
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