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http://dx.doi.org/10.3795/KSME-A.2007.31.10.1031

A Study on the Development of Control Loading System for Helicopter Flight Training Device  

Han, Dong-Ju ((주)대한항공 항공기술연구원)
Lee, Sang-Haeng ((주)썬에어로시스)
Publication Information
Transactions of the Korean Society of Mechanical Engineers A / v.31, no.10, 2007 , pp. 1031-1038 More about this Journal
Abstract
A study on the development of control loading system for a pilot command in the helicopter flight training device is performed. The key issue of the device is how to provide closely the real feeling of the stick forces to the trainer during the flight training. Focusing on this proviso and considering the suitable approach than the complexity of the hydraulic system, we adopt the AC servo motor system although its inherent disadvantages such as the torque ripple and the stick-slip friction effect at a low control force. However, we overcome these detrimental effects by introducing the appropriate control device and the robust structural design of the actuating system, thereby the feasibility and applicability to the system can be obtained by showing good performance, meeting the required specification.
Keywords
Helicopter Flight Training Device; Control Loading System;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
Times Cited By SCOPUS : 0
연도 인용수 순위
1 Qiang. F, Yu. Y. and Xiao. C. W., 2005, 'Disturbance Observer Design for Electric Aerodynamic Load Simulator,' Proceedings of the Fourth International Conference on Machine Learning and Cybernetics, Guangzhou
2 FAA AC 120-63, 'Helicopter Simulator Qualification. '
3 FAA AC 120-45A, 'Airframe Flight Training Device Standards.'
4 CASA Order 2004-49, 'Specified Standard and Inspection Essentials for Flight Training Device.'
5 Chan-Seok Lee and Byoung-Soo Kim, 2004, 'Research on the Design and Evaluation of a Control Loading System for Flight Simulator', The Korean Society for Aeronautical and Space Sciences, Vol. 32, pp. 95-100
6 Fokker, 1998, 'ECol 8000/4000 Fokker Electrical CLS User Manual.'
7 Jai-Hyuk Hwang and Seong-Choon Lee, 1996, 'Analysis of Force Control Characteristics of Control Loading System of a Flight Simulator,' The Korean Society for Aeronautical and Space Sciences, Vol. 24, pp. 4146-4155
8 Zhao. H. Y., Jian. D. W. and Jiong. H. T., 2003, 'Hybrid Control of Load Simulator for Unmanned Aerial Vehicle Based on Wavelet Networks,' Proceedings of the Second International Conference on Machine Learning and Cybernetics, Xi 'an
9 Kyung-Ho Bang, 1998, 'Robust $\mu$-Controller Design of Control Loading System for Aircraft Simulator,' The Korean Society of Electronic Engineers, Autumn Conference, Vol. 21, pp. 405-408
10 Yun-Soo Nam, 2001, 'Analysis of Dynamic Characteristics for Flight Load Simulator,' The Korean Society of Mechanical Engineers, Part A, Vol. 25, pp. 478-485
11 Jai-Hyuk Hwang, Dae-Seung Park, Young-Su Kim and Duk-Su Kang, 1996, 'Computation of Stick Forces for Control Loading System of Flight Simulator,' The Korean Society for Aeronautical and Space Sciences, Vol. 24, pp. 3088-3097