Aircraft Ground Braking Assistant Control Based on Pilot Control Model

被引：2

作者：

Dai, Yaqi ^{[1
]}

Yu, Liangyao ^{[1
]}

Song, Jian ^{[1
]}

Abi, Lanie ^{[1
]}

Zheng, Sheng ^{[1
]}

机构：

[1] Tsinghua Univ, Dept Automot Engn, Beijing 100084, Peoples R China

来源：

IEEE ACCESS | 2020年 / 8卷

基金：

美国国家科学基金会;

关键词：

Atmospheric modeling; Aircraft; Aerospace control; Vehicle dynamics; Visualization; Biological system modeling; Real-time systems; Aircraft ground braking; pilot assistant control; pilot-aircraft system; real time simulation; linear parameter variant; SYSTEMS ADAS; NETWORK;

D O I：

10.1109/ACCESS.2020.2993173

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Aircraft ground braking control is a complex time-varying dynamic problem, especially when there are unexpected disturbances from lateral wind or visual error. Therefore, under some extreme conditions, it is hard for the pilot to control aircraft braking as well as usual without assistant control. This paper solves this problem by proposing a novel assistant control for aircraft ground braking, mainly based on the pilot control model and the LPV theory. And in order to reflect the control characteristics of the pilot, the sensory and control-theoretic model were combined together for controller designing. To test the performance of proposed control method, a real time pilot-in-loop simulation system is constructed. According to experiment results, the proposed assistant control shows better performance than pilot control, for it not only help the pilot to resist disturbance, but also hardly run counter to the pilot & x2019;s intent.

引用

页码：88643 / 88650

页数：8

共 27 条

[1] SELF-SCHEDULED H-INFINITY CONTROL OF LINEAR PARAMETER-VARYING SYSTEMS - A DESIGN EXAMPLE [J].

APKARIAN, P ;

GAHINET, P ;

BECKER, G .

AUTOMATICA, 1995, 31 (09) :1251-1261

[2]

Boril J., 2012, P 15 INT C MECHATRON, P1

[3] The lateral control during aircraft-on-ground deceleration phases [J].

Dai, Yaqi ;

Song, Jian ;

Yu, Liangyao ;

Lu, Zhenghong ;

Zheng, Sheng ;

Li, Fei .

AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 95

[4]

Güvenç BA, 2001, P AMER CONTR CONF, P13, DOI 10.1109/ACC.2001.945506

[5] Simplified approach for modelling pilot pursuit control behaviour in multi-loop flight control tasks [J].

Hess, R. A. .

PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2006, 220 (G2) :85-102

[6]

Jeon JW, 2004, IEEE IND ELEC, P1710

[7] The Dynamic Pilot Behavioral Models [J].

Jirgl, Miroslav ;

Havlikova, Marie ;

Bradac, Zdenek .

25TH DAAAM INTERNATIONAL SYMPOSIUM ON INTELLIGENT MANUFACTURING AND AUTOMATION, 2014, 2015, 100 :1192-1197

[8] AN OPTIMAL CONTROL MODEL OF HUMAN RESPONSE .1. THEORY AND VALIDATION [J].

KLEINMAN, DL ;

BARON, S ;

LEVISON, WH .

AUTOMATICA, 1970, 6 (03) :357-&

[9]

Lavretsky E., 2008, SYSTEM IDENTIFICATIO

[10] Review of pilot models used in aircraft flight dynamics [J].

Lone, Mudassir ;

Cooke, Alastair .

AEROSPACE SCIENCE AND TECHNOLOGY, 2014, 34 :55-74

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