Based on the bifurcation analysis and Catastrophe theory methodology (BACTM), the aircraft global dynamic stability in rapid rolling maneuver is studied in this paper.
本文应用分支和突变理论，研究飞机在状态参数和操纵参数组成的空间内急滚机动全局稳定性。
2
The study will provide a new theoretical approach to investigate aircraft agility, the direct force control and post-stall maneuver of modern combat aircraft.
为飞机敏捷性、直接力控制和过失速机动问题提供了一种理论研究方法。
3
The longitudinal and lateral directional control effectiveness requirements of high maneuveraircraft are discussed in this paper, and the fighter J-7 is taken as an example.