The results show that the effects of aerodynamic moment characteristics, elevator control law, and pilot mathematical model parameters on the deep-stall characteristics are considerable.

• 研究结果表明,气动力矩特性、升降舵操纵规律和驾驶员模型参数的变化对“T”型尾翼飞机的深失速改出特性有显著的影响。