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

^*Corresponding author for this work

School of Automation Science and Electrical Engineering

Beihang University

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

17 Scopus citations

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.

Original language	English
Title of host publication	2006 IEEE Conference on Robotics, Automation and Mechatronics
DOIs	https://doi.org/10.1109/RAMECH.2006.252621
State	Published - 2006
Event	2006 IEEE Conference on Robotics, Automation and Mechatronics - Bangkok, Thailand Duration: 7 Jun 2006 → 9 Jun 2006

Publication series

Name	2006 IEEE Conference on Robotics, Automation and Mechatronics

Conference

Conference	2006 IEEE Conference on Robotics, Automation and Mechatronics
Country/Territory	Thailand
City	Bangkok
Period	7/06/06 → 9/06/06

Keywords

Anti-skid current
Braking rectification
Friction coefficient
Side wind
Slip ratio

Access to Document

10.1109/RAMECH.2006.252621

Cite this

@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. in 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, Thailand, 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

Abstract

Publication series

Conference

Keywords

Access to Document

Other files and links

Fingerprint

Cite this