Title:
航空機のステアリング角制御システム
Document Type and Number:
Japanese Patent JP5608918
Kind Code:
B2
Abstract:
To provide an aircraft steering angle control system that minimizes the amount of skidding of an airframe that is turning on a low-µ taxiway surface such as an icy taxiway surface and allows for directional control of the airframe by a steering command, an aircraft steering angle control system that outputs an operation signal related to a steering angle S as a control command signal for a nose steering wheel incorporates a nose wheel envelope protection 4 including a reference steering angle setting unit 41 that calculates a reference steering angle S s on the assumption that the airframe is not skidding; a skid detection unit 42 that detects a skidding state of the airframe based on the reference steering angle S s ; and a switch unit 43 that selects a control command signal for a nose wheel in conjunction with the skid detection unit 42.
Inventors:
舩引 浩平
新川 智子
山口 恭弘
山路 拓郎
新川 智子
山口 恭弘
山路 拓郎
Application Number:
JP2009147211A
Publication Date:
October 22, 2014
Filing Date:
June 22, 2009
Export Citation:
Assignee:
独立行政法人 宇宙航空研究開発機構
三菱重工業株式会社
三菱重工業株式会社
International Classes:
B64C25/50
Attorney, Agent or Firm:
Oshiro Shigenobu
Masuo Yamada
Masuo Yamada