The spacecraft autonomous control system is compared with the traditional spacecraft control system.
对自主运行和传统测控方式进行了比较。
A control method with sliding mode of nonlinear spacecraft system is provided in this paper, in which the interactive influences among channels of strong nonlinear spacecraft system are decoupled.
提出了非线性空间飞行器系统采用滑动模态控制方法，它对强非线性的空间飞行器系统通道间交叉影响进行解耦。
The control system consists of some controlling hardware, a set of sensors, and a set of actuators for controlling the spacecraft.
控制系统包含了一些控制硬件、一组感测器、以及一组用来控制航空器的促动器。
The star sensor is a measuring unit used for providing information to the attitude control system on spacecraft .
星敏感器是为空间飞行器姿态控制系统提供姿态信息的测量系统。
Reaction wheel is one of the main disturbance sources for the attitude control system accuracy of spacecraft.
反作用轮是影响航天器姿态控制系统精度的主要扰动源之一。
In this paper, the basic theory of the inverse system method is introduced, and is used in the design of a spacecraft attitude control system.
本文首先介绍了逆系统方法的基本思想，然后将其用于航天器非线性姿态控制系统的设计中。
To study the attitude system of spacecraft, an adaptive inverse control algorithm is presented.
针对航天器姿态系统，提出了一种基于自适应神经网络动态逆的控制算法。
According to the requirements of modern spacecraft control, this paper presents a hierarchical intelligent adaptive control system based on the description of plant feature model knowledge.
针对现代航天器对控制任务的需求特点，基于航天器对象特征模型知识描述，提出了具有多层结构的智能自适应控制系统概念。
The proposed results are useful to the attitude dynamic analysis and control system design for not only the spacecraft with large rotation parts, but also the agile small satellite.
所得结果不仅适用于具有大型运动部件的航天器的姿态动力学分析及控制系统设计，也适用于灵敏小卫星的相应研究。
Reaction wheel is one of the main disturbance sources that affect the precision of attitude control system of spacecraft.
反作用轮是影响航天器姿态控制系统精度的主要扰动源之一。
The results indicate that the mini thermoelectric heat pump-PCM thermal control system can provide effective thermal control of high power spacecraft electronics.
结果表明，采用该热控系统对航天器短时大功率组件进行温度控制是可行的。
The relation among parameters is derived and the stability of single axis flexible spacecraft attitude control system is studied.
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。
When designing the attitude control system of spacecraft, it is necessary to take account of the sunlight pressure disturbance torques under various sunlight incident conditions.
在设计航天器姿控系统时，需要充分考虑各种光照条件下航天器所受到的太阳光压干扰力矩。
Reaction wheel assembly is one of the main disturbances affecting the accuracy of attitude control system in the spacecraft.
反作用轮系统是影响航天器姿控系统精度的主要扰动源之一。
In this paper, the robustness stability analysis of the attitude control system of a three-axis stabilized flexible spacecraft is investigated.
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。
Reaction wheel is one of the main disturbance sources that affect the precision of attitude control system of spacecraft.
反作用轮系统是影响航天器姿控系统精度的主要扰动源之一。
Based on the results, a normal matrix design approach for spacecraft attitude control systems is developed by using a feedback perturbation description for system uncertainties.
基于正规性分析结果，使用系统不确定性反馈摄动描述对姿态控制系统的正规矩阵设计方法进行研究。
In this paper, the control of coordinated motion of spacecraft attitude and the end-effector of a free-floating space-based robot system is discussed.
本文讨论了载体姿态受控、位置不受控制的漂浮基空间机器人协调运动的控制问题。
Objective To deal with the mass optimization of thermal control system as well as environmental control and life support system(ECLSS) of manned spacecraft.
目的解决载人航天器热控和环控生保系统的轻量化问题。
This article deals with torque allocation for redundant flywheel configurations in a spacecraft attitude control system.
主要研究了航天器姿控系统中冗余飞轮构型的力矩分配问题。
This paper analyzes the characteristics of Spacecraft Fault Diagnosis System and the basic idea and principle of Role-Based Access Control model.
文章介绍了基于角色的权限管理模型的基本思想及工作原理，并分析了航天器故障诊断系统中权限管理的特征。
Reaction wheel is one of the main disturbance sources for the attitude control system accuracy of spacecraft.
反作用轮系统是影响航天器姿控系统精度的主要扰动源之一。
Reaction wheel is one of the main disturbance sources that affect the precision of attitude control system of spacecraft.
实现了用直流力矩电机在反作用飞轮控制方式下对气球吊篮的方位控制。
Reaction wheel is one of the main disturbance sources for the attitude control system accuracy of spacecraft.
反作用轮微振动是影响卫星姿态控制精度的重要因素。
Reaction wheel is one of the main disturbance sources that affect the precision of attitude control system of spacecraft.
反作用飞轮是卫星姿态控制系统的重要执行元件，提高飞轮系统的性能对卫星姿态控制系统具有重要意义。
A novel heat pump ice thermal storage integration scheme based on reducing total mass (including relative power system mass) of thermal control system of spacecraft is presented.
提出了旨在降低热控系统质量的热泵-蓄冷组合热控方案。
A novel heat pump ice thermal storage integration scheme based on reducing total mass (including relative power system mass) of thermal control system of spacecraft is presented.
提出了旨在降低热控系统质量的热泵-蓄冷组合热控方案。
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