Interceptor attitude control system is a nonlinear control system.
拦截器姿态控制系统是一个非线性控制系统。
An example of an attitude control system of a bending vehicle is given.
文中给出了一个弹性飞行器的姿态控制系统作为设计举例。
The attitude control system designed with this concept has better flexibility.
用这种方案设计的姿态控制系统有非常好的灵活性。
As an application example, its application to flight attitude control system is analysed.
作为应用实例，分析了在飞行姿态控制系统中的应用。
The algorithm has been embedded in the attitude control system of a small unmanned helicopter.
该算法已应用于小型无人直升机的姿态控制中。
The integrated power and attitude control for a bias momentum attitude control system is investigated.
研究偏置动量姿态控制系统中的集成能量与姿态控制问题。
The attitude Control System (ACS) software is responsible for maintaining the attitude of the spacecraft.
姿态控制系统(acs)软体负责维护航空器的姿态。
Generally, magnetic suspending flywheel and ordinary fly wheel are adopted in the attitude control system.
一般的卫星姿态控制都采用飞轮控制方案，所采用的飞轮有磁悬浮飞轮和普通飞轮两种。
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。
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。
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 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。
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。
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。
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。
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