An evaluation model for control effector superiority based on performance requirements

Yan Liu; Zhenghong Gao

An evaluation model for control effector superiority based on performance requirements

Yan Liu, Zhenghong Gao

School of Aeronautics

Northwestern Polytechnical University Xian

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

1 Scopus citations

Abstract

To simplify the control allocation design, a quantitative evaluation model for over-actuated aircrafts is proposed based on performance requirements. The flight requirements of different flight phases, including beyond visual range (BVR), within visual range (WVR), takeoff and landing, are analyzed. Quantitative evaluation models of control effector superiority of different flight phases are proposed. Control effector superiority parameters and flight performance indices of a typical over-actuated aircraft are evaluated. The simulation results show that the flight performance results coincide with the control effector superiority results, which indicates the control effector evaluation model is reasonable and effective.

Original language	English
Title of host publication	29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014
Publisher	International Council of the Aeronautical Sciences
ISBN (Electronic)	3932182804
State	Published - 2014
Event	29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014 - St. Petersburg, Russian Federation Duration: 7 Sep 2014 → 12 Sep 2014

Publication series

Name	29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014

Conference

Conference	29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014
Country/Territory	Russian Federation
City	St. Petersburg
Period	7/09/14 → 12/09/14

Keywords

Control allocation
Control effector superiority
Flight performance
Over-actuated aircraft

Cite this

@inproceedings{913e7802b5e04b2a84e0ac2607e9f4d7,

title = "An evaluation model for control effector superiority based on performance requirements",

abstract = "To simplify the control allocation design, a quantitative evaluation model for over-actuated aircrafts is proposed based on performance requirements. The flight requirements of different flight phases, including beyond visual range (BVR), within visual range (WVR), takeoff and landing, are analyzed. Quantitative evaluation models of control effector superiority of different flight phases are proposed. Control effector superiority parameters and flight performance indices of a typical over-actuated aircraft are evaluated. The simulation results show that the flight performance results coincide with the control effector superiority results, which indicates the control effector evaluation model is reasonable and effective.",

keywords = "Control allocation, Control effector superiority, Flight performance, Over-actuated aircraft",

author = "Yan Liu and Zhenghong Gao",

year = "2014",

language = "英语",

series = "29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014",

publisher = "International Council of the Aeronautical Sciences",

booktitle = "29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014",

note = "29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014 ; Conference date: 07-09-2014 Through 12-09-2014",

}

Liu, Y & Gao, Z 2014, An evaluation model for control effector superiority based on performance requirements. in 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014. 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014, International Council of the Aeronautical Sciences, 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014, St. Petersburg, Russian Federation, 7/09/14.

An evaluation model for control effector superiority based on performance requirements. / Liu, Yan; Gao, Zhenghong.
29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014. International Council of the Aeronautical Sciences, 2014. (29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014).

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

TY - GEN

T1 - An evaluation model for control effector superiority based on performance requirements

AU - Liu, Yan

AU - Gao, Zhenghong

PY - 2014

Y1 - 2014

N2 - To simplify the control allocation design, a quantitative evaluation model for over-actuated aircrafts is proposed based on performance requirements. The flight requirements of different flight phases, including beyond visual range (BVR), within visual range (WVR), takeoff and landing, are analyzed. Quantitative evaluation models of control effector superiority of different flight phases are proposed. Control effector superiority parameters and flight performance indices of a typical over-actuated aircraft are evaluated. The simulation results show that the flight performance results coincide with the control effector superiority results, which indicates the control effector evaluation model is reasonable and effective.

AB - To simplify the control allocation design, a quantitative evaluation model for over-actuated aircrafts is proposed based on performance requirements. The flight requirements of different flight phases, including beyond visual range (BVR), within visual range (WVR), takeoff and landing, are analyzed. Quantitative evaluation models of control effector superiority of different flight phases are proposed. Control effector superiority parameters and flight performance indices of a typical over-actuated aircraft are evaluated. The simulation results show that the flight performance results coincide with the control effector superiority results, which indicates the control effector evaluation model is reasonable and effective.

KW - Control allocation

KW - Control effector superiority

KW - Flight performance

KW - Over-actuated aircraft

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M3 - 会议稿件

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BT - 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014

PB - International Council of the Aeronautical Sciences

T2 - 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014

Y2 - 7 September 2014 through 12 September 2014

ER -

An evaluation model for control effector superiority based on performance requirements

Abstract

Publication series

Conference

Keywords

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