Research on Distributed Interactive Simulation Method of Missiles Attitude Control System;
研究航天器集成能量与姿态控制系统中飞轮的控制律。
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。
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 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。
The primary node is responsible for running the communications subsystems and the attitude control system code.
主要节点负责执行通讯子系统与姿态控制系统。
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。
The problems concerning an aerospace vehicle's(ASV) atmospheric reentry flight attitude control system were researched.
研究了空天飞行器（ASV）再入跨大气层飞行时的姿态控制问题。
Now, flywheels systems are elected as the actuators of attitude control system with high precision for most spacecrafts.
目前空间飞行器的高精度姿态控制系统大多采用飞轮系统。
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。
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。
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。
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。
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 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。
Maneuverable warhead are the complex nonlinear system, which take a great challenge to the attitude control system designers.
机动弹头是复杂的非线性系统，它给姿态控制系统设计人员以极大的挑战。
This VS control law implements robust control of attitude control system, at the same time, it overcome the chattering problem.
该变结构控制律在实现姿态控制系统鲁棒控制的同时，有效地抑制了传统变结构控制的抖振现象。
The control, technology of wheel state feedback is the. leading topic of the actuator in the satellite attitude control system.
飞轮状态反馈控制技术是当前卫星姿控系统执行部件的前沿课题。
The stratospheric nacelle attitude control system is the key technology in keeping position stabilization and posture adjustment.
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 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。
The experimental results show that the testing model is reasonable, and can reflect the modes of attitude control system correctly.
实验表明，所建立的测试系统模型是合理的，能够正确反映姿态控制系统的工作模态。
According to the classical control theory, this paper deals with two designs of critical statically unstable attitude control system.
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。
This VS control law implements robust control of attitude control system, at the same time, it overcomes the traditional chattering problem.
该变结构控制律在实现姿态控制系统鲁棒控制的同时，有效地抑制了传统变结构控制的抖振现象。
As a kind of high accuracy executive machine, reaction wheel has been extensively applied to the attitude control system (ACS) of satellites.
作为一种高精度的执行机构，反作用飞轮已广泛应用于卫星姿态控制系统中。
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。
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。
In this paper an advanced design concept of zero-bias momentum 3-axes attitude control system consisting of four skew reaction wheels is presented.
本文提出一个与常规不同的零动量——偏置动量三轴姿态控制系统的设计方案。该系统由四个斜装的反作用轮组成。
Simultaneously, the study for gimbal magnetic suspension momentum wheel can benefit the integrated power and attitude control system technologically.
同时，万向磁悬浮动量轮的研究也为集成能源与姿态控制系统的研究提供了技术支持。
The simulation results shows that lateral attitude control system has good control performance and the auto-trim control strategy plays a effective role.
仿真验证结果表明，抗不确定干扰的横侧向姿态控制回路控制性能良好，自动配平控制策略能有效发挥作用。
In view of the particularity for maneuver warhead reentry trajectory and the guidance method, key techniques in attitude control system design are analyzed.
针对机动弹头再入弹道和制导方式的特殊性，分析了激光末制导机动弹头姿控系统设计的关键技术。
The paper introduces simply the knowledge-based tolerance attitude control system. The project idea for implementing the control in a class of vehicle is presented.
本文对知识基故障容错姿态控制系统加以简单的介绍。并对一类运载器提出实现它的方案设想。
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