Study of helicopter autorotation landing following engine failure based on a six-degree-of-freedom rigid-body dynamic model

Author:

Meng Wanli,Chen Renliang

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference21 articles.

1. Johnson W. Helicopter optimal descent and landing after power loss. Report No.: NASA TM-73244; 1977.

2. Optimal landing of a helicopter in autorotation;Lee;J Guid Control Dyn,1988

3. Optimal autorotational descent of a helicopter with control and state inequality constraints;Lee;J Guid Control Dyn,1990

4. Floros MW. Descent analysis for rotorcraft survivability with power loss. In: Proceedings of the American helicopter society 65th annual forum; 2009. p. 2633–46.

5. Chen RTN, Zhao Y. Optimal trajectories for the helicopter in one-engine-inoperative terminal-area operations. Report No.: NASA TM-110400; 1996.

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