| 摘要 |
PCT No. PCT/GB95/00990 Sec. 371 Date Oct. 28, 1996 Sec. 102(e) Date Oct. 28, 1996 PCT Filed May 1, 1995 PCT Pub. No. WO95/30180 PCT Pub. Date Nov. 9, 1995A stabilization system is disclosed in which stabilization pitch and roll signals effective for stabilizing the aircraft are combined with respective pilot provided elevator and aileron position demand signals in accordance with a function which reduces the effects of the stabilizing signals in dependence on increasing values of the respective elevator and aileron position demand signals. |
