A Force Control Test Rig for the Dynamic Characterization of Helicopter Primary Flight Control Systems-Reference-Cited by-同舟云学术

A Force Control Test Rig for the Dynamic Characterization of Helicopter Primary Flight Control Systems

Published:2015 Issue: Volume:106 Page:71-82
ISSN:1877-7058
Container-title:Procedia Engineering
language:en
Short-container-title:Procedia Engineering

Author:

Bertucci Alessandro,Mornacchi Andrea,Jacazio Giovanni,Sorli Massimo

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference9 articles.

1. Jacazio, G., and Balossini, G., (2009). “A Mechatronic Active Force Control System for Real Time Test Loading of an Aircraft Landing Gear”. In Proceedings of the ASME 2009 International Design Engineering Technical Conferences & Computers and Information in Engineering Conference IDETC/CIE 2009, San Diego, August 30-September 2.

2. Jacazio, G., and Balossini, G., (2007). “Real-time Loading Actuator Control for an Advanced Aerospace Test Rig”. In Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering 2009.

3. Jacazio, G., and Balossini, G., (2008). “The Iron Bird for M346 Advanced Trainer”. In SAE A6 Meeting on Aerospace Fluid Power and Actuation Systems, Portland, USA, October 13-16. .

4. J. A. Ferreira, F. Gomes de Almeida, M.R. Quintas, (2002).“Semi-empirical model for a hydraulic servo-solenoid valve” Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering May 1, 2002 vol. 216 no. 3 237-248.

5. D. C. Pountney, W. Weston. M. R. Baineghbal, (1989).“A numerical study of turbulent flow characteristic of Servo-Valve orifices” Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy May 1989 vol. 203 no. 2 139-147.

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