Mathematical model and characteristic analysis of return trajectory for lunar probe were studied.
对月球探测器的返回轨道进行了建模与特性分析。
According to the task, must design a standard return trajectory which is reference trajectory for guidance when a manned spacecraft returns.
载人航天器返回时，根据任务的要求，需要设计一条标准返回轨道，作为制导时的参考轨道。
If the trajectory is correct, the spacecraft will pass close to the moon and swings back into space to return to earth.
如果轨道正确，宇宙飞船会在月球附近通过，并飞回太空以返回地球。
The chaotic trajectory of the controlled 4-D system can be controlled to return to its zero balance point under different initial conditions.
在不同的初始条件下，所设计的控制器可以将受控四维混沌系统的混沌轨道很快控制到系统的零平衡点。
The chaotic trajectory of the controlled 4-D system can be controlled to return to its zero balance point under different initial conditions.
在不同的初始条件下，所设计的控制器可以将受控四维混沌系统的混沌轨道很快控制到系统的零平衡点。
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