当机器人缓步走向椅子并坐下来时，系统软件此时计算出机器人为保持稳定、充分利用桌子而采取的若干姿态。
The software then calculates a number of poses that the robot could strike to make best use of the table for stability while it shuffles towards the chair and sits on it.
活系统将它们的不稳定姿态传染给它们接触到的任何事物，而且它们无所不及。
Vivisystems spread their poised instability into whatever they touch, and they reach for everything.
气球吊篮姿态控制系统是吊篮在空中保持姿态稳定、进行姿态调整的关键部件。
The stratospheric nacelle attitude control system is the key technology in keeping position stabilization and posture adjustment.
在拖曳速度为6～9节的情况下，能够控制拖曳系统按预定轨迹进行波浪运动，同时保持较稳定的姿态。
The towed vehicle could fly along the desired track and keep the steady attitude under 6~9 knots speed.
本论文分别以三轴稳定刚性卫星姿态控制和带太阳帆板的三轴稳定卫星姿态控制为研究对象，建立了控制系统数学模型。
Models of the three-axis stabilized Attitude Control Systems of a rigid satellite and a flexible satellite with a pair of solar arrays are set up.
最后，该文设计了一个基于PC机的三轴稳定卫星姿态控制硬件在回路仿真系统，将反作用飞轮、陀螺等实物接入仿真系统。
At last, the hardware in the loop simulation system for three-axis stabilized satellite attitude control based on PC, with reaction wheel and gyro in the loop is designed.
根据经典控制理论，设计了两类临界静不稳定姿态控制系统。
According to the classical control theory, this paper deals with two designs of critical statically unstable attitude control system.
基于古典控制理论和BTT倾斜转弯控制技术，设计了可重复使用运载器(RLV)的大气层内姿态稳定控制系统。
Focused on the problem of reusable launch vehicle (RLV) attitude control, an engineering attitude control system based on the classical control theory and BTT technology was designed.
本文应用区间矩阵的理论，研究三轴稳定的挠性空间飞行器姿态控制系统的鲁棒稳定性分析问题。
In this paper, the robustness stability analysis of the attitude control system of a three-axis stabilized flexible spacecraft is investigated.
推导系统参数间的关系式，分析挠性空间飞行器主轴姿态控制系统稳定性问题。
The relation among parameters is derived and the stability of single axis flexible spacecraft attitude control system is studied.
结果表明，稳定和控制是足够的，飞行品质满意后稳定性增强，滚动姿态保护系统的工作原理。
The results show that the stability and control are sufficient, that the flying qualities are satisfactory after stability augmentation, and that the roll attitude protection system works as expected.
结果表明，稳定和控制是足够的，飞行品质满意后稳定性增强，滚动姿态保护系统的工作原理。
The results show that the stability and control are sufficient, that the flying qualities are satisfactory after stability augmentation, and that the roll attitude protection system works as expected.
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