Research on modeling and simulation of aircraft taxiing rectification

Li Bo; Jiao Zongxia; Wang Shaoping

doi:10.1109/RAMECH.2006.252621

Research on modeling and simulation of aircraft taxiing rectification

Li Bo^*
, Jiao Zongxia
, Wang Shaoping

^*此作品的通讯作者

自动化科学与电气工程学院

Beihang University

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

17 引用（Scopus）

摘要

For ideal condition, applied the same brake instruction signals to the aircraft right and left brake devices, the main wheels brake synchronously, and the aircraft doesn't yaw. Whereas considering the side wind, the asymmetry of brake devices and the differences between tire and course coefficients, the aircraft may yaw. By analyzing the causations of aircraft deviation from the course during taxiing, the aircraft dynamic model with side wind is built, and a kind of differential braking control law based on slip ratio is proposed. Simulation results show that, by introducing this law the difference of brake tire velocities is eliminated, thereby aircraft can run along the correct course.

源语言	英语
主期刊名	2006 IEEE Conference on Robotics, Automation and Mechatronics
DOI	https://doi.org/10.1109/RAMECH.2006.252621
出版状态	已出版 - 2006
活动	2006 IEEE Conference on Robotics, Automation and Mechatronics - Bangkok, 泰国期限: 7 6月 2006 → 9 6月 2006

出版系列

姓名	2006 IEEE Conference on Robotics, Automation and Mechatronics

会议

会议	2006 IEEE Conference on Robotics, Automation and Mechatronics
国家/地区	泰国
市	Bangkok
时期	7/06/06 → 9/06/06

访问文件

10.1109/RAMECH.2006.252621

其它文件与链接

链接到 Scopus 的出版物

引用此

@inproceedings{0a7c5de8322a4d08bfa71daeb6f29515,

title = "Research on modeling and simulation of aircraft taxiing rectification",

abstract = "For ideal condition, applied the same brake instruction signals to the aircraft right and left brake devices, the main wheels brake synchronously, and the aircraft doesn't yaw. Whereas considering the side wind, the asymmetry of brake devices and the differences between tire and course coefficients, the aircraft may yaw. By analyzing the causations of aircraft deviation from the course during taxiing, the aircraft dynamic model with side wind is built, and a kind of differential braking control law based on slip ratio is proposed. Simulation results show that, by introducing this law the difference of brake tire velocities is eliminated, thereby aircraft can run along the correct course.",

keywords = "Anti-skid current, Braking rectification, Friction coefficient, Side wind, Slip ratio",

author = "Li Bo and Jiao Zongxia and Wang Shaoping",

year = "2006",

doi = "10.1109/RAMECH.2006.252621",

language = "英语",

isbn = "1424400244",

series = "2006 IEEE Conference on Robotics, Automation and Mechatronics",

booktitle = "2006 IEEE Conference on Robotics, Automation and Mechatronics",

note = "2006 IEEE Conference on Robotics, Automation and Mechatronics ; Conference date: 07-06-2006 Through 09-06-2006",

}

Bo, L, Zongxia, J & Shaoping, W 2006, Research on modeling and simulation of aircraft taxiing rectification. 在 2006 IEEE Conference on Robotics, Automation and Mechatronics., 4018736, 2006 IEEE Conference on Robotics, Automation and Mechatronics, 2006 IEEE Conference on Robotics, Automation and Mechatronics, Bangkok, 泰国, 7/06/06. https://doi.org/10.1109/RAMECH.2006.252621

TY - GEN

T1 - Research on modeling and simulation of aircraft taxiing rectification

AU - Bo, Li

AU - Zongxia, Jiao

AU - Shaoping, Wang

PY - 2006

Y1 - 2006

N2 - For ideal condition, applied the same brake instruction signals to the aircraft right and left brake devices, the main wheels brake synchronously, and the aircraft doesn't yaw. Whereas considering the side wind, the asymmetry of brake devices and the differences between tire and course coefficients, the aircraft may yaw. By analyzing the causations of aircraft deviation from the course during taxiing, the aircraft dynamic model with side wind is built, and a kind of differential braking control law based on slip ratio is proposed. Simulation results show that, by introducing this law the difference of brake tire velocities is eliminated, thereby aircraft can run along the correct course.

AB - For ideal condition, applied the same brake instruction signals to the aircraft right and left brake devices, the main wheels brake synchronously, and the aircraft doesn't yaw. Whereas considering the side wind, the asymmetry of brake devices and the differences between tire and course coefficients, the aircraft may yaw. By analyzing the causations of aircraft deviation from the course during taxiing, the aircraft dynamic model with side wind is built, and a kind of differential braking control law based on slip ratio is proposed. Simulation results show that, by introducing this law the difference of brake tire velocities is eliminated, thereby aircraft can run along the correct course.

KW - Anti-skid current

KW - Braking rectification

KW - Friction coefficient

KW - Side wind

KW - Slip ratio

UR - https://www.scopus.com/pages/publications/34547371176

U2 - 10.1109/RAMECH.2006.252621

DO - 10.1109/RAMECH.2006.252621

M3 - 会议稿件

AN - SCOPUS:34547371176

SN - 1424400244

SN - 9781424400249

T3 - 2006 IEEE Conference on Robotics, Automation and Mechatronics

BT - 2006 IEEE Conference on Robotics, Automation and Mechatronics

T2 - 2006 IEEE Conference on Robotics, Automation and Mechatronics

Y2 - 7 June 2006 through 9 June 2006

ER -

Research on modeling and simulation of aircraft taxiing rectification

摘要

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会议

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