Based on the principleofflight of fan wing aircraft, realizing methods of VTOL are preposed by changing the Angle of attack and increasing chord length of the tail.
In this paper, the method of reentry maneuver guidance applying to attack the ground fixed target is described by using flight dynamics principle and modern control theory.
本文运用飞行力学原理和现代控制理论,对攻击地面固定目标的飞行器的再入机动制导方法进行了研究。
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This paper analyzes hydrostatic servo actuator in motion system for flight simulator, and introduces structural principleof main component of the system.