FLIGHT CONTROL LAWS FOR VERTICAL FLIGHT PATH CONTROL
摘要
<p>A flight control system and method for controlling the vertical flight path of an aircraft, the flight control system includes a stable decoupled model having a decoupled lateral equation of motion and a decoupled longitudinal equation of motion and a feedback command loop operably associated with the stable decoupled model. The feedback command loop includes a vertical flight path angle control law; an altitude control law; and a vertical speed control law.</p>
申请公布号
WO2012096668(A1)
申请公布日期
2012.07.19
申请号
WO2011US21225
申请日期
2011.01.14
申请人
BELL HELICOPTER TEXTRON INC.;CHRISTENSEN, KEVIN, THOMAS;SHUE, SHYHPYNG, JACK;CAUDILL, TROY, SHELDON