Modification of a Helicopter Inverse Simulation to Include an Enhanced Rotor Model-Reference-Cited by-同舟云学术

Modification of a Helicopter Inverse Simulation to Include an Enhanced Rotor Model

Published:2000-05 Issue:3 Volume:37 Page:536-538
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Doyle Sharon A.¹,Thomson Douglas G.¹

Affiliation:

1. Glasgow University, Glasgow, Scotland G12 8QQ, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.2633

Reference4 articles.

1. Helicopter Inverse Simulation Incorporating an Individual Blade Rotor Model

2. Generalized technique for inverse simulation applied to aircraft maneuvers

3. 4Rutherford, S. “Simulation Techniques for the Study of the Manoeuvring of Advanced Rotorcraft Configurations,” Ph.D. Dissertation, Dept. of Aerospace Engineering,Univ. of Glasgow, Glasgow, Scotland, U.K.March 1997.

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