( 2 ) transient jet - interaction phenomena , challenge project , is analyzed by computational unsteady aerodynamic method . boundary condition of transient jet is established ( 2 )将非定常空气动力学数值计算方法创造性地应用于姿态控制发动机瞬态流场计算。
To solve this problem , we propose an output feedback control law without angular velocities by making use of the inherent passivity of the attitude control system 针对这种情况，本文利用刚体姿态控制系统中固有的无源性，设计了无需角速率测量值的刚体姿态控制器。
4 . the three - axis attitude stabilization system of the flexible satellite has been studied , in which three basic vibration modes of the solar array have been considered 4 、在挠性卫星动力学模型的基础上，建立了只考虑太阳帆板三阶振动模态的挠性卫星三轴姿态控制模型。
Satellite attitude determination system is the important part of the attitude control system ( acs ) , and its accuracy is the key factor for the performance of the acs 卫星姿态确定系统是卫星姿态控制系统中的重要组成部分,其精度是影响姿态控制系统精度水平的决定性因素。
In the article , a self - learning stochastic method based on the statistical pattern recognition is presented for attitude control under the disturbance of blind mixed gaussian white noises 摘要本文提出一种基于统计模式识别，针对盲混合高斯白噪声干扰下卫星姿态控制的方法。
The thesis tracks the research about the intercept technology oversea . the rolling missile model with attitude - control - system is established by referring to the figuration dimension of pac - 3 本文跟踪国外研究，以“爱国者? 3 ”导弹外形尺寸为参考建立了具有姿态控制系统的滚转导弹模型。
The attitude control algorithm is based on dynamic inverse control method . the algorithm is adaptable , with the use of neural network compensating the error between the model and the real helicopter 姿态控制算法采用动态逆控制方法,并利用神经网络在线补偿模型误差,使其具有自适应能力。
Active vibration control technique is the key technology of designing of attitude control system for large flexible spacecraft to fulfill mission requirements such as precision pointing and integrity of structures 航天器挠性结构的主动振动控制技术是大型航天器姿态控制系统设计的关键技术。
As a key section of microsatellite , the microsatellite attitude control system should have the feature of simple configuration , light weight , long working time and high reliability 作为现代微小卫星关键部分，现代微小卫星的姿态控制系统需具有结构简单、质量轻、工作时间长和可靠性高的特点。
The wind tunnel " s control system is a large and complicated system , which including three set control system : mach number system , model attitude system , compressor surveillance - control system 该风洞控制系统较为庞大复杂，共有三套系统：马赫数控制系统、模型姿态控制系统和压缩机控制系统。
