Analytical Synthesis of Stabilization Laws for Spacecraft Orbit Attitude Using Information on an Angle and the Full Vector of Angular Velocity

N. E. Zubov; E. A. Mikrin; V. N. Ryabchenko; I. V. Sorokin

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Analytical Synthesis of Stabilization Laws for Spacecraft Orbit Attitude Using Information on an Angle and the Full Vector of Angular Velocity

机译：使用关于角速度的角度和完整向量的航天器轨道态度稳定法的分析综合

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摘要

The problem of stabilizing the spacecraft orbit attitude was solved analytically for the sixth order model of its rotary motion with the use of the output feedback control synthesis that is based on decomposition of a control object. Numerical simulation data are presented.

机译：通过使用基于对照对象的分解的输出反馈控制合成来分析稳定航天器轨道态度的问题。提供了数值模拟数据。

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来源
《Russian Aeronautics》 |2018年第2期|共11页
作者
N. E. Zubov; E. A. Mikrin; V. N. Ryabchenko; I. V. Sorokin;
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作者单位

Bauman Moscow State Technical University;

Korolev Rocket and Space Corporation Energiya;

Bauman Moscow State Technical University;

Korolev Rocket and Space Corporation Energiya;

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原文格式 PDF
正文语种 eng
中图分类航空;
关键词
MIMO-system; spacecraft; output control; orbital stabilization;

机译：MIMO系统;航天器;输出控制;轨道稳定;

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专利

1. Analytical Synthesis of Stabilization Laws for Spacecraft Orbit Attitude Using Information on an Angle and the Full Vector of Angular Velocity [J] . N. E. Zubov, E. A. Mikrin, V. N. Ryabchenko, Russian Aeronautics . 2018,第2期

机译：使用关于角速度的角度和完整向量的航天器轨道态度稳定法的分析综合
2. L_2 Disturbance Attenuation Control for Input Saturated Spacecraft Attitude Stabilization without Angular Velocity Measurements [J] . Bing Xiao, Qinglei Hu, Aihua Zhang International Journal of Control, Automation, and Systems . 2012,第1期

机译：输入角饱和航天器姿态稳定的L_2扰动衰减控制，无需角速度测量
3. L₂ disturbance attenuation control for input saturated spacecraft attitude stabilization without angular velocity measurements [J] . Bing Xiao, Qinglei Hu, Aihua Zhang International Journal of Control, Automation and Systems . 2012,第1期

机译：L _{2 干扰衰减控制，用于在不进行角速度测量的情况下输入饱和航天器的姿态稳定}
4. Angular Velocity-Free Control for Rigid Spacecraft Attitude Stabilization under Input Constraint [C] . Bing Xiao, Qinglei Hu, Youmin Zhang IFAC World Congress . 2011

机译：输入限制下刚性航天器姿态稳定的角速度控制
5. Attitude dynamics and stability of a flexible gravity-gradient stabilized spacecraft in orbit raising maneuvers. [D] . Chen, Shih-Chieh. 2000

机译：柔性重力梯度稳定航天器在升轨道中的姿态动力学和稳定性。
6. Joint angles and angular velocities and relevance of eigenvectors during prehension in the monkey [O] . Jodi F. Prosise, Claudia M. Hendrix, Timothy J. Ebner -1

机译：猴子抓握过程中的联合角和角速度及其特征向量的相关性
7. Defining the Spacecraft Angular Position in the Orbital Stabilization Mode from the Angular Rate Sensor Measurements [O] . A. S. Oleynik, N. E. Zubov, V. N. Ryabchenko 2015

机译：从角速率传感器测量中定义轨道稳定模式中的航天器角位置

Analytical Synthesis of Stabilization Laws for Spacecraft Orbit Attitude Using Information on an Angle and the Full Vector of Angular Velocity

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