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Study of helicopter autorotation landing following engine failure based on a six-degree-of-freedom rigid-body dynamic model |
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| Authors: | Meng Wanli Chen Renliang |
| Institution: | Science and Technology Laboratory on Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics,Nanjing 210016, China |
| Abstract: | |
| Keywords: | Autorotation landing Engine failure Helicopters Optimal control Rigid-body model |
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