The conception of the flight quasi steadystatemotion and the design method based on it are proposed in the characteristic of the large amplitude maneuvering of the fighter.
根据战斗机大幅值机动运动特点,提出了准稳态运动概念及其设计方法。
2
The results shown that, with the effect of nonlinear components, the symmetry of rotation trajectory of the bearing center was broken, and the motion of the journal center presented a steadystate.