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本文在参考文献[1]的基础上,研究飞机线性加(减)速时纵向角运动的稳定性,获得了角运动渐近稳定的充分条件.
Based on the reference [1], this paper studies the stability of the longitudinal angular motion when the aircraft is linearly added (decelerated) and obtains sufficient conditions for the asymptotic stability of the angular motion.