Affiliation:
1. Embry-Riddle Aeronautical University
Publisher
American Institute of Aeronautics and Astronautics
Reference43 articles.
1. Johnson, W. “Helicopter Optimal Descent and Landing After Power Loss,” Tech. Rep. 19770019123, NASA, 1977.
2. Dooley, L., and Yeary, R. “Flight Test Evaluation of the High Inertia Rotor System,” Tech. Rep. ADA071648, Bell Helicopter Textron, June 1979.
3. Lee, A. “Optimal Landing of a Helicopter in Autorotation,” Ph.D. thesis,Stanford University, 1985.
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1 articles.
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