Low Speed Turning Flight Path Control of a STOL Aircraft

摘要

This paper is concerned with an automatic low speed turning flight path control system design for a STOL aircraft. A flight control system is designed using an approximate perfect servo, which is effective to the control of non-minimum phase plant. A complementary input method which will reduce the control errors of this servo system is introduced. Favourable simulation results are obtained which will substantiate the effectiveness of present methods.