Experiment and study of control loading system in a flight simulator based on RCP

Zheng Shutao; Huang Qitao; Cong Dacheng; Han Junwei

doi:10.1109/ICITECHNOLOGY.2007.4290462

Experiment and study of control loading system in a flight simulator based on RCP

Zheng Shutao, Huang Qitao, Cong Dacheng, Han Junwei

Harbin Institute of Technology

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

12 Scopus citations

Abstract

Control loading system is one of the important components for a flight simulator. It provides fidelity force simulation to pilot and belongs to passive force control system. According to the flight control system's principle of boeing737-300, this paper gives the simulation principle in flight simulator. Three channels Primary Control Loading system (PCL) hydraulic driven actuators were developed. The mathematical model was derived for the PCL. By means of rapid control prototyping technology, the passive force control system based on industrial personal computer is developed. Experiments demonstrate that the system has less than 4% error between computed force and actual force and good tracking performance. The PCL has been applied to flight simulator prototype system.

Original language	English
Title of host publication	IEEE ICIT 2007 - 2007 IEEE International Conferenceon Integration Technology
Pages	208-212
Number of pages	5
DOIs	https://doi.org/10.1109/ICITECHNOLOGY.2007.4290462
State	Published - 2007
Externally published	Yes
Event	2007 IEEE International Conference on Integration Technology, ICIT 2007 - Shenzhen, China Duration: 20 Mar 2007 → 24 Mar 2007

Publication series

Name	IEEE ICIT 2007 - 2007 IEEE International Conference on Integration Technology

Conference

Conference	2007 IEEE International Conference on Integration Technology, ICIT 2007
Country/Territory	China
City	Shenzhen
Period	20/03/07 → 24/03/07

Keywords

Control loading system
Flight simulator
Passive force control system
Rapid control prototyping

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10.1109/ICITECHNOLOGY.2007.4290462

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Shutao, Z., Qitao, H., Dacheng, C., & Junwei, H. (2007). Experiment and study of control loading system in a flight simulator based on RCP. In IEEE ICIT 2007 - 2007 IEEE International Conferenceon Integration Technology (pp. 208-212). Article 4290462 (IEEE ICIT 2007 - 2007 IEEE International Conference on Integration Technology). https://doi.org/10.1109/ICITECHNOLOGY.2007.4290462

@inproceedings{880804674c154f99ba697df7d1939187,

title = "Experiment and study of control loading system in a flight simulator based on RCP",

abstract = "Control loading system is one of the important components for a flight simulator. It provides fidelity force simulation to pilot and belongs to passive force control system. According to the flight control system's principle of boeing737-300, this paper gives the simulation principle in flight simulator. Three channels Primary Control Loading system (PCL) hydraulic driven actuators were developed. The mathematical model was derived for the PCL. By means of rapid control prototyping technology, the passive force control system based on industrial personal computer is developed. Experiments demonstrate that the system has less than 4% error between computed force and actual force and good tracking performance. The PCL has been applied to flight simulator prototype system.",

keywords = "Control loading system, Flight simulator, Passive force control system, Rapid control prototyping",

author = "Zheng Shutao and Huang Qitao and Cong Dacheng and Han Junwei",

year = "2007",

doi = "10.1109/ICITECHNOLOGY.2007.4290462",

language = "英语",

isbn = "1424410924",

series = "IEEE ICIT 2007 - 2007 IEEE International Conference on Integration Technology",

pages = "208--212",

booktitle = "IEEE ICIT 2007 - 2007 IEEE International Conferenceon Integration Technology",

note = "2007 IEEE International Conference on Integration Technology, ICIT 2007 ; Conference date: 20-03-2007 Through 24-03-2007",

}

Shutao, Z, Qitao, H, Dacheng, C & Junwei, H 2007, Experiment and study of control loading system in a flight simulator based on RCP. in IEEE ICIT 2007 - 2007 IEEE International Conferenceon Integration Technology., 4290462, IEEE ICIT 2007 - 2007 IEEE International Conference on Integration Technology, pp. 208-212, 2007 IEEE International Conference on Integration Technology, ICIT 2007, Shenzhen, China, 20/03/07. https://doi.org/10.1109/ICITECHNOLOGY.2007.4290462

Experiment and study of control loading system in a flight simulator based on RCP. / Shutao, Zheng; Qitao, Huang; Dacheng, Cong et al.
IEEE ICIT 2007 - 2007 IEEE International Conferenceon Integration Technology. 2007. p. 208-212 4290462 (IEEE ICIT 2007 - 2007 IEEE International Conference on Integration Technology).

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

TY - GEN

T1 - Experiment and study of control loading system in a flight simulator based on RCP

AU - Shutao, Zheng

AU - Qitao, Huang

AU - Dacheng, Cong

AU - Junwei, Han

PY - 2007

Y1 - 2007

N2 - Control loading system is one of the important components for a flight simulator. It provides fidelity force simulation to pilot and belongs to passive force control system. According to the flight control system's principle of boeing737-300, this paper gives the simulation principle in flight simulator. Three channels Primary Control Loading system (PCL) hydraulic driven actuators were developed. The mathematical model was derived for the PCL. By means of rapid control prototyping technology, the passive force control system based on industrial personal computer is developed. Experiments demonstrate that the system has less than 4% error between computed force and actual force and good tracking performance. The PCL has been applied to flight simulator prototype system.

AB - Control loading system is one of the important components for a flight simulator. It provides fidelity force simulation to pilot and belongs to passive force control system. According to the flight control system's principle of boeing737-300, this paper gives the simulation principle in flight simulator. Three channels Primary Control Loading system (PCL) hydraulic driven actuators were developed. The mathematical model was derived for the PCL. By means of rapid control prototyping technology, the passive force control system based on industrial personal computer is developed. Experiments demonstrate that the system has less than 4% error between computed force and actual force and good tracking performance. The PCL has been applied to flight simulator prototype system.

KW - Control loading system

KW - Flight simulator

KW - Passive force control system

KW - Rapid control prototyping

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M3 - 会议稿件

AN - SCOPUS:46449106450

SN - 1424410924

SN - 9781424410927

T3 - IEEE ICIT 2007 - 2007 IEEE International Conference on Integration Technology

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EP - 212

BT - IEEE ICIT 2007 - 2007 IEEE International Conferenceon Integration Technology

T2 - 2007 IEEE International Conference on Integration Technology, ICIT 2007

Y2 - 20 March 2007 through 24 March 2007

ER -

Experiment and study of control loading system in a flight simulator based on RCP

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