FLIGHT CONTROL SYSTEM HAVING A THREE CONTROL LOOP DESIGN
摘要
<p>A flight control system is configured for controlling the flight of an aircraft utilizing a three control loop design to robustly increase system performance. An inner loop comprises an improved linear quadratic regulator (LQR) search method, and an outer loop comprises a classic feedback summary gain design. A third loop comprises a steady state trim search method.</p>
申请公布号
WO2007018572(A2)
申请公布日期
2007.02.15
申请号
WO2005US40394
申请日期
2005.11.08
申请人
BELL HELICOPTER TEXTRON INC.;SHUE, SHYHPYNG, JACK;SCHILLINGS, JOHN, J.