The method of intelligent control applied to the orbital control of rendezvous and docking phase of spacecraft is presented in this paper.
本文介绍了将智能控制方法用于航天器交会对接段的轨道控制。
After the taikonauts had returned to Earth, the BX-1 was placed under active control and commanded to maneuver back towards the orbital module, which had been left in orbit.
宇航员返回地球之后，BX - 1实施了主动控制，并通过命令向留在轨道上的轨道舱返回。
These droids would blindly obey orders spoken to them by their commanders or transmitted to them from an orbital Droid Control ship.
这些机器人盲从于指挥官亲口下达或轨道机器人控制舰传输的命令。
This time will employ manual control method by the astronauts working in the orbital station to achieve docking from the orbital station.
这一次将采用由在轨道站上工作的宇航员从轨道站上进行人工控制实现对接的方式。
An orbital modulation method by controlling the corresponding transient orbit errors of mean orbit control targets was proposed.
提出了一种通过控制平均轨道控制目标对应的瞬时轨道偏差量进行轨道修正的方法。
This paper considers the minimum-time control of aeroassisted orbital transfer vehicle (AOTV) which arises in the study of coplanar HEO-LEO orbital transfer.
本文研究了在共面圆轨道HEO-LEO的过程中，气动辅助轨道转移飞行器（AOTV）在大气内飞行的极小时间控制问题。
The attitude control law is designed for the orbital maneuver with considering the output character of the attitude control thrusters.
根据姿态控制推力器的输出特性，设计了轨道控制期间卫星姿态控制方案。
Then the paper applies EA and SPEA to an orbital transformation problem. - time-energy optimization o The paper also solve low thrust control problem of relative motion using fuzzy logic.
然后分别用一般的进化算法和改进的SPEA方法解决轨道转移的时间-能量优化问题，对于相对运动方程有限推力控制问题，本文用模糊控制的方法加以解决。
Electrodynamic tethers with low thrust-to-weight ratios can only perform orbital transfers over a large number of revolutions, which poses a real challenge to short time scale optimal control methods.
电动力绳系卫星的推力幅值较小且方向固定，完成轨道机动任务的周期长，其最优控制问题的求解比较困难。
Finally, the orbital elements are introduced as state variables and the accelerations are produced by equation as control variables, the space interception model is established.
最后，采用轨道根数作为状态变量，以航天器发动机产生的推力加速度作为控制变量建立空间拦截模型。
When the satellite takes orbital maneuver, the control force may stimulate the vibration of the flexible appendages and, therefore, affects the attitude of the satellite.
卫星轨道控制期间，轨道控制推力会激振挠性太阳帆板，从而也影响卫星的姿态。
Up to now the singular optimal control problems in the thrust synergetic orbital transfer have not been completely solved.
特别是由推力协同变轨所导致的奇异最优控制问题到目前尚没有完全解决。
The optimization performance index is to maximize the orbital plane change, and the optimal lift and bank control law are obtained.
以目标轨道面倾角最大为优化性能指标，获得了升力和滚转角的最优控制规律。
The optimization performance index is to maximize the orbital plane change, and the optimal lift and bank control law are obtained.
以目标轨道面倾角最大为优化性能指标，获得了升力和滚转角的最优控制规律。
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