Design and flight testing of various controllers for the Bell 205 helicopter-Reference-Cited by-同舟云学术

Design and flight testing of various controllers for the Bell 205 helicopter

Published:2005-03 Issue:3 Volume:13 Page:383-398
ISSN:0967-0661
Container-title:Control Engineering Practice
language:en
Short-container-title:Control Engineering Practice

Author:

Postlethwaite Ian,Prempain Emmanuel,Turkoglu Ercument,Turner Matthew C.,Ellis Kris,Gubbels A.W.

Publisher

Elsevier BV

Subject

Applied Mathematics,Electrical and Electronic Engineering,Computer Science Applications,Control and Systems Engineering

Reference20 articles.

1. Anonymous, (2000). Handling qualities requirements for military rotorcraft, aeronautical design standard ADS-33E-PRF. U.S. Army Aviation and Missile Command, Aviation Engineering Directorate, Redstone Arsenal, Alabama.

2. Baillie, S. W., Morgan, M. J., & Goheen, K. (1995). Practical experiences in control system design using the NRC Bell 205 airborne simulator. AGARD conference proceedings 560, actice control technology: applications and lessons learned (pp. 27.1–27.12).

3. Digital re-design of the Bell 205 airborne simulator artificial feel system;Gubbels;Canadian Aeronautics and Space Journal,1997

4. Hoh, R. H., Mitchell, D. G., & Aponso, B. L. (1989). Background information and user's guide for handling requirements for military rotorcraft. USAAVSCOM technical report 89-A-008.

5. Howell, S., & McCallum, A. (2001). Private communication.

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