Modal control of an electrohydrostatic flight simulator motion system

Andrew R Plummer, Paolo Serena Guinzio

Research output: Chapter in Book/Report/Conference proceedingChapter

11 Citations (Scopus)

Abstract

Valve-controlled electro-hydraulic actuators in a Stewart platform configuration have become established as a good way of meeting the performance required for flight simulator motion systems. However, valve-controlled actuators are very inefficient, and thus an electrohydrostatic motion system, controlled using servomotor driven pumps, has been developed by Thales, and is now in production. This paper presents a simulation study of a multi-axis controller which can improve the dynamic response of the new motion system. A modal control approach is used - i.e. the modes of vibration of the system are controlled individually. These modes are dependent on the inertial properties of the platform and the compliance of the actuators. The modes change as the motion system moves throughout its workspace, and so the controller has to adapt to the current operating point. Simulation results are presented based on a partially validated model of the motion system.
Original languageEnglish
Title of host publicationProceedings of the ASME Dynamic Systems and Control Conference 2009, DSCC2009
Place of PublicationNew York
PublisherAmerican Society of Mechanical Engineers (ASME)
Pages1257-1264
Number of pages8
VolumeB
ISBN (Electronic)978-0-7918-3860-0
ISBN (Print)9780791848920
DOIs
Publication statusPublished - 2010
Event2009 ASME Dynamic Systems and Control Conference, DSCC2009, October 12, 2009 - October 14, 2009 - Hollywood, CA, USA United States
Duration: 1 Jan 2010 → …

Conference

Conference2009 ASME Dynamic Systems and Control Conference, DSCC2009, October 12, 2009 - October 14, 2009
CountryUSA United States
CityHollywood, CA
Period1/01/10 → …

Fingerprint

Flight simulators
Actuators
Hydraulic actuators
Servomotors
Controllers
Dynamic response
Pumps
Compliance

Cite this

Plummer, A. R., & Guinzio, P. S. (2010). Modal control of an electrohydrostatic flight simulator motion system. In Proceedings of the ASME Dynamic Systems and Control Conference 2009, DSCC2009 (Vol. B, pp. 1257-1264). [DSCC2009-2608] New York: American Society of Mechanical Engineers (ASME). https://doi.org/10.1115/DSCC2009-2608

Modal control of an electrohydrostatic flight simulator motion system. / Plummer, Andrew R; Guinzio, Paolo Serena.

Proceedings of the ASME Dynamic Systems and Control Conference 2009, DSCC2009. Vol. B New York : American Society of Mechanical Engineers (ASME), 2010. p. 1257-1264 DSCC2009-2608.

Research output: Chapter in Book/Report/Conference proceedingChapter

Plummer, AR & Guinzio, PS 2010, Modal control of an electrohydrostatic flight simulator motion system. in Proceedings of the ASME Dynamic Systems and Control Conference 2009, DSCC2009. vol. B, DSCC2009-2608, American Society of Mechanical Engineers (ASME), New York, pp. 1257-1264, 2009 ASME Dynamic Systems and Control Conference, DSCC2009, October 12, 2009 - October 14, 2009, Hollywood, CA, USA United States, 1/01/10. https://doi.org/10.1115/DSCC2009-2608
Plummer AR, Guinzio PS. Modal control of an electrohydrostatic flight simulator motion system. In Proceedings of the ASME Dynamic Systems and Control Conference 2009, DSCC2009. Vol. B. New York: American Society of Mechanical Engineers (ASME). 2010. p. 1257-1264. DSCC2009-2608 https://doi.org/10.1115/DSCC2009-2608
Plummer, Andrew R ; Guinzio, Paolo Serena. / Modal control of an electrohydrostatic flight simulator motion system. Proceedings of the ASME Dynamic Systems and Control Conference 2009, DSCC2009. Vol. B New York : American Society of Mechanical Engineers (ASME), 2010. pp. 1257-1264
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