发明申请
- 专利标题: STEERING ANGLE CONTROL SYSTEM FOR AIRCRAFT
- 专利标题(中): 转向角度控制系统
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申请号: US13378473申请日: 2010-06-22
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公开(公告)号: US20120158218A1公开(公告)日: 2012-06-21
- 发明人: Kohei Funabiki , Tomoko Shinkawa , Yasuhiro Yamaguchi , Takuro Yamaji
- 申请人: Kohei Funabiki , Tomoko Shinkawa , Yasuhiro Yamaguchi , Takuro Yamaji
- 优先权: JP2009-147211 20090622
- 国际申请: PCT/JP2010/060501 WO 20100622
- 主分类号: B64C25/50
- IPC分类号: B64C25/50
摘要:
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 as a control command signal for a nose steering wheel incorporates a nose wheel envelope protection including a reference steering angle setting unit that calculates a reference steering angle on the assumption that the airframe is not skidding; a skid detection unit that detects a skidding state of the airframe based on the reference steering angle; and a switch unit that selects a control command signal for a nose wheel in conjunction with the skid detection unit.
公开/授权文献
- US08874285B2 Steering angle control system for aircraft 公开/授权日:2014-10-28
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