发明名称 Roll attitude-dependent roll rate limit
摘要 Systems and methods are provided for a roll attitude dependent roll rate limit that may limit an aircraft to a lower roll rate limit under normal flight conditions. The 5 systems and methods may detect situations where a higher roll rate limit may be desirable and allow the aircraft to exceed the lower roll rate limit, to either a higher roll rate limit or a roll rate between the lower and higher roll rate limit. - 31 - 420 | 430 | 440 Airplane State Sensors: Pilot Controls: Autopilot Roll Rate Control Wheel Bank Angle Pedal Flap Position Airspeed Altitude Pitch Attitude , F450 Flight Control Computer Vehicle Dynamic Characteristic Calculation Roll Rate Regulation and Surface Command Calculation Flight Control Actuators and Roll Control Surfaces: Ailerons Flaperons Spoilers Rudders
申请公布号 AU2016204312(A1) 申请公布日期 2017.03.30
申请号 AU20160204312 申请日期 2016.06.24
申请人 The Boeing Company 发明人 Wilson, Douglas L.;Grubb, David W.;Morel, Mark R.
分类号 B64C13/16;B64C13/50;B64C17/00 主分类号 B64C13/16
代理机构 代理人
主权项
地址