摘要
本文用BACTM法配合时域动态响应研究了JJ-6飞机进入和改出尾旋的操纵规律.文中所用的操纵面是方向舵和升降舵。通过计算、分析,确定出可能出现尾旋的操纵区。最后探讨了尾旋进入和改出的机理。
In this paper, based on the Bifurcation Analysis and Catastrophe Theory Methodology (BACTM) combining with the check of time history the control laws of spin entry and recovery have been studied. The control surfaces used in the control system are a rudder and an elevator.The region occuring spin has been determined by using the approach proposed in this paper. The mechanism of spin entry and recovery have been explored.
出处
《飞行力学》
CSCD
北大核心
1989年第4期15-27,共13页
Flight Dynamics
