轨道保持(orbit keeping) 利用航天器上的动力装置调整航天器的速度,修正轨道参数,使航天器运行轨道与标准轨道的偏离量限制在给定范围内(常以星下点的偏离值来表征)。对不同高度的航天器,轨道保持的方法也不相同。
According as the need of satellites orbital keeping request, orbital keeping project is brought forward. It can be guaranteed that the satellites' longitude and latitude excursion will always keep less than the given value.
根据卫星轨道保持的要求,提出位置保持方案,使卫星偏离定点位置的经纬漂移量小于给定值。
参考来源 - 卫星智能自主控制系统的研究But it’s difficult to carry out this method of orbit keeping, because it needs strict requirements on celestial bodies period and calculating accuracy.
但是,用这种控制策略对四体问题中的航天器进行轨道保持,大天体的运动周期和计算上的精度有严格的要求,在现实中不容易实现。
参考来源 - Halo轨道编队飞行的摄动分析·2,447,543篇论文数据,部分数据来源于NoteExpress
研究了编队飞行的控制系统结构和共线拉格朗日点附近的周期轨道保持控制问题。
Secondly, the control system structure and station keeping problems near collinear Lagrange points are studied.
基于微分修正算法给出了一种简单的拟周期轨道保持控制方法,数值仿真表明该方法具有较高的控制效率。
A simple station keeping control algorithm is given based on differential corrections, and numerical simulation shows that the algorithm is very effective.
它可以让火车在现有蜿蜒盘旋的轨道上保持匀速。
It allows the train to maintain a constant speed through the twists and turns of existing track.
And the third fact that we need to keep in mind is that spins remain parallel prior to adding a second electron in any of the orbitals.
第三个事实是我们需要记住在,每个轨道加入第二个电子之前,自旋保持平行。
I am going to say if that electron is to stay in its orbit, that is to say it doesn't flee the atom, it doesn't collapse under the nucleus then the sum of the forces on the electron must be zero No net force. And so that will be the sum of a dynamic force plus an electrostatic.
如果电子会保持在它的轨道上运行,既不脱离原子的话,它就不会由于原子核对它的吸引力而被瓦解掉,电子所受的合力一定为零,由于没有合力,所以电子所受力为动态力和静电力的总和。
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