Sliding mode control with angular acceleration feedback for a flight motion simulator

Ma Jie; Yao Yu; Liu Ka

doi:10.1109/SSST.2009.4806818

Sliding mode control with angular acceleration feedback for a flight motion simulator

Ma Jie^*
, Yao Yu
, Liu Ka

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

2 Scopus citations

Abstract

Control system architecture will help eliminate or reduce non-linear behavior of flight motion simulator axes motions. This elimination and reduction will help improve dynamic transparency in HWIL simulations. The control strategy proposed in this paper combines the sliding mode control and the angular acceleration feedback to suppress the influence of payload variation, nonlinear friction and external disturbance torque. The test results indicate this approach significantly improves the simulator performance and presents an effective routine to produce the high fidelity flight motion simulator.

Original language	English
Title of host publication	2009 IEEE International Symposium on Sustainable Systems and Technology, ISSST 2009
Pages	190-194
Number of pages	5
DOIs	https://doi.org/10.1109/SSST.2009.4806818
State	Published - 2009
Event	2009 IEEE International Symposium on Sustainable Systems and Technology, ISSST 2009 - Tullahoma, TN, United States Duration: 15 Mar 2009 → 17 Mar 2009

Publication series

Name	2009 IEEE International Symposium on Sustainable Systems and Technology, ISSST 2009

Conference

Conference	2009 IEEE International Symposium on Sustainable Systems and Technology, ISSST 2009
Country/Territory	United States
City	Tullahoma, TN
Period	15/03/09 → 17/03/09

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10.1109/SSST.2009.4806818

Cite this

@inproceedings{340422efa71c41c7b20428ee43c3fd3b,

title = "Sliding mode control with angular acceleration feedback for a flight motion simulator",

abstract = "Control system architecture will help eliminate or reduce non-linear behavior of flight motion simulator axes motions. This elimination and reduction will help improve dynamic transparency in HWIL simulations. The control strategy proposed in this paper combines the sliding mode control and the angular acceleration feedback to suppress the influence of payload variation, nonlinear friction and external disturbance torque. The test results indicate this approach significantly improves the simulator performance and presents an effective routine to produce the high fidelity flight motion simulator.",

author = "Ma Jie and Yao Yu and Liu Ka",

year = "2009",

doi = "10.1109/SSST.2009.4806818",

language = "英语",

isbn = "9781424433254",

series = "2009 IEEE International Symposium on Sustainable Systems and Technology, ISSST 2009",

pages = "190--194",

booktitle = "2009 IEEE International Symposium on Sustainable Systems and Technology, ISSST 2009",

note = "2009 IEEE International Symposium on Sustainable Systems and Technology, ISSST 2009 ; Conference date: 15-03-2009 Through 17-03-2009",

}

Jie, M, Yu, Y & Ka, L 2009, Sliding mode control with angular acceleration feedback for a flight motion simulator. in 2009 IEEE International Symposium on Sustainable Systems and Technology, ISSST 2009., 4806818, 2009 IEEE International Symposium on Sustainable Systems and Technology, ISSST 2009, pp. 190-194, 2009 IEEE International Symposium on Sustainable Systems and Technology, ISSST 2009, Tullahoma, TN, United States, 15/03/09. https://doi.org/10.1109/SSST.2009.4806818

Sliding mode control with angular acceleration feedback for a flight motion simulator. / Jie, Ma; Yu, Yao; Ka, Liu.
2009 IEEE International Symposium on Sustainable Systems and Technology, ISSST 2009. 2009. p. 190-194 4806818 (2009 IEEE International Symposium on Sustainable Systems and Technology, ISSST 2009).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

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AU - Jie, Ma

AU - Yu, Yao

AU - Ka, Liu

PY - 2009

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N2 - Control system architecture will help eliminate or reduce non-linear behavior of flight motion simulator axes motions. This elimination and reduction will help improve dynamic transparency in HWIL simulations. The control strategy proposed in this paper combines the sliding mode control and the angular acceleration feedback to suppress the influence of payload variation, nonlinear friction and external disturbance torque. The test results indicate this approach significantly improves the simulator performance and presents an effective routine to produce the high fidelity flight motion simulator.

AB - Control system architecture will help eliminate or reduce non-linear behavior of flight motion simulator axes motions. This elimination and reduction will help improve dynamic transparency in HWIL simulations. The control strategy proposed in this paper combines the sliding mode control and the angular acceleration feedback to suppress the influence of payload variation, nonlinear friction and external disturbance torque. The test results indicate this approach significantly improves the simulator performance and presents an effective routine to produce the high fidelity flight motion simulator.

UR - https://www.scopus.com/pages/publications/67649519809

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DO - 10.1109/SSST.2009.4806818

M3 - 会议稿件

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SN - 9781424433254

T3 - 2009 IEEE International Symposium on Sustainable Systems and Technology, ISSST 2009

SP - 190

EP - 194

BT - 2009 IEEE International Symposium on Sustainable Systems and Technology, ISSST 2009

T2 - 2009 IEEE International Symposium on Sustainable Systems and Technology, ISSST 2009

Y2 - 15 March 2009 through 17 March 2009

ER -

Sliding mode control with angular acceleration feedback for a flight motion simulator

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