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本文用BACTM理论配合时域动态响应研究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副翼和升降舵。通过计算、分析,确定出可能出现尾旋的操纵区,最后探讨了进入和改出尾旋的机理.
In this paper, the control law of JJ-6 aircraft entering and changing out of the tail rotation is studied by using BACTM theory and time-domain dynamic response.The control surfaces used in this paper are aileron and elevator. Through calculation and analysis, the control zone with possible tail rotation can be determined. Finally, the mechanism of entering and changing tail rotation is discussed.