Paper Title:
Investigation and Application of the Helicopter Typical Flight States Identification
  Abstract

Typical flight states are the most important checking items during the helicopter flight-test. This article intends to illustrate the typical flight states identification method via introducing the basic theory and characteristics of helicopter control, and then apply this method to load analysis and compilation of loads spectrum.

  Info
Periodical
Edited by
Zeyong Yin, Chengyu Jiang, Datong Qin, Peixin Qiao and Geng Liu
Pages
556-561
DOI
10.4028/www.scientific.net/AMM.86.556
Citation
Z. H. Wan, "Investigation and Application of the Helicopter Typical Flight States Identification", Applied Mechanics and Materials, Vol. 86, pp. 556-561, 2011
Online since
August 2011
Authors
Export
Price
$32.00
Share

In order to see related information, you need to Login.

In order to see related information, you need to Login.

Authors: Xue Mei Yu, An Ping Zhao, Xue Li
Chapter 3: Design Science, Dynamics Systems and Applied Mechanics Applications
Abstract:A method which can process flight test data by integrating parameter identification and non-dimensional flight dynamic model was proposed to...
246
Authors: Shu Xun Zhou, Jie An, Jian Guo Yao, Fei Hu
Chapter 6: Mechatronics and Robotics Technology
Abstract:Autonomous helicopter flight presents challenges in flight control system design with scalability. In this paper, we present the integration...
718
Authors: Xue Mei Yu, Hua Zhang, Wen Jun Zhao
Chapter 4: Measurements, Instrumentation, Testing, Monitoring, Analysis and Detection Technologies
Abstract:Method to deal flight test data on take-off performance for light aircrafts was provided in this paper. Firstly, the corresponding flight...
1084