attitude dynamics

Development of the simulation software platform for satellite orbit and attitude dynamics

卫星轨道姿态动力学仿真软件平台研究与开发

The attitude dynamics and kinematics of small satellite are analysed .

分析了小卫星的姿态动力学及运动学方程；

The Attitude Dynamics and Control of Large Space Structure

大型空间结构姿态动力学和控制

Modeling and Control of Attitude Dynamics of a Space Station with Changing Structure

变构型空间站的姿态动力学建模与控制

Attitude dynamics model and control of liquid filled flexible spacecraft

挠性充液卫星姿态动力学建模研究

The model of spacecraft attitude dynamics and the attitude control technology are generalized .

对航天器姿态动力学模型和姿态控制技术进行了概括和总结。

Relative Attitude Dynamics and Control in Satellite Formation Flying

卫星编队飞行相对姿态动力学与控制

Methods of large-scale systems and satellite attitude dynamics

大系统方法与卫星姿态动力学

Simulation Framework for Spacecraft Attitude Dynamics and Control Based on Matlab / Simulink

基于Matlab/Simulink的航天器姿态动力学与控制仿真框架

The two algorithms do not use information of relative attitude dynamics between spacecrafts .

两种算法都不需要编队卫星间的姿态动力学联系。

Study on attitude dynamics of a liquid filled spacecraft with manipulators

带空间机械臂的充液航天器姿态动力学研究

In one methods , the attitude dynamics is used only to propagate the attitude rate .

其中一种方法是采用姿态动力学模型进行姿态角速度的递推。

Nonlinear Plane Vibrations in the Attitude Dynamics of Artificial Satellite

人造卫星姿态动力学中的非线性平面振动

Attitude dynamics and control of a flexible multi-body satellite

挠性多体卫星姿态动力学与控制

Attitude dynamics of solar wings on spacecraft with a flexible shaft

带挠性轴太阳帆板航天器姿态动力学研究

Research on Attitude Dynamics Modeling and Control for Spin-Stabilized Micro-Satellite

自旋小卫星姿态动力学建模与控制研究

The error between satellite attitude dynamics and its linearized model can affect the attitude control precision .

卫星姿态动力学系统与其线性化模型之间的误差会影响姿态控制的精度。

A mathematical model derived from spacecraft attitude dynamics is treated as an example to demonstrate its application .

以一个呈现混沌姿态运动的航天器动力学模型为例说明了该控制律的应用。

Study on attitude dynamics of a liquid-filled spacecraft with elastic appendages

带弹性伸展附件充液航天器姿态动力学研究

The attitude dynamics of a satellite with flexible appendages

带弹性附件的卫星的姿态动力学方程

Pitching attitude dynamics modeling and its control of unmanned dirigible airship

自主飞艇俯仰角姿态动力学建模及控制

The satellite attitude dynamics function is established , that is disturbed by the first-order Markov force moment .

建立了卫星受一阶马尔柯夫干扰力矩时的卫星姿态动力学方程；

The Attitude Dynamics and Control of On-Orbit Refueling Spacecrafts

航天器在轨加注的姿态动力学与控制

Attitude dynamics and control of dual-spin satellites

双自旋卫星的姿态运动和控制

Attitude Dynamics and Control Simulation for RVD Target-Spacecraft

交会对接目标飞行器姿态动力学与控制仿真研究

With PD and optimal control of classical control theory model of the spacecraft attitude dynamics modeling , and conducted a detailed MATLAB simulation .

并用PD及最优控制等经典控制理论对航天器姿态动力学模型进行了建模，并运用MATLAB进行了详细的仿真，得到了仿真结果。

Topics extend to analysis of both aircraft flight dynamics and spacecraft attitude dynamics , based upon presented principles and equations of motion .

课题扩展分析了航天器飞行动力学和太空船飞行姿态动力学，这些建立在当前的运动理论和方程式上。

First , the modified rodrigues parameters ( MRP ) were adopted to describe the attitude dynamics of spacecraft ;

首先，采用修正的罗德里格斯参数描述航天器姿态动力学；

On the basis of this , an affine attitude dynamics model is established and the attitude control law is designed by using backstepping control method .

以此为基础，建立了仿射型姿态运动模型，利用退步方法设计了控制律；

A new configuration of mass moment missile is presented with the in-depth analysis of attitude dynamics model , which can ensure that the system has better dynamic quality .

通过对姿态动力学模型的深入分析，获得了一种使系统具备良好动态品质的构型。