Adaptive robust sliding mode simultaneous control of spacecraft attitude and micro-vibration based on magnetically suspended control and sensitive gyro

Yuan Ren; Xiaocen Chen; Yuanwen Cai; Weijie Wang; Qiang Liu

首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers >Adaptive robust sliding mode simultaneous control of spacecraft attitude and micro-vibration based on magnetically suspended control and sensitive gyro

【24h】

Adaptive robust sliding mode simultaneous control of spacecraft attitude and micro-vibration based on magnetically suspended control and sensitive gyro

机译：基于磁悬浮控制和敏感陀螺的航天器姿态和微振动的自适应鲁棒滑模同时控制

获取原文

获取原文并翻译 | 示例

掌桥外文数据库（机构版） >>

开具论文收录证明 >>

文献代查 >>

页面导航

摘要
著录项
相似文献
相关主题

摘要

This paper puts forward realizing the synchronous control of spacecraft attitude and micro-vibration by taking advantage of magnetic suspension rotor deflection of magnetically suspended control and sensitive gyro. A disturbance-observer is designed to estimate the complex micro vibration which is hard to measure, and an adaptive robust sliding mode controller is designed as an integrated controller and its stability is proven by Lyapunov stability criterion. The band-pass filters are introduced to separate low frequency and high frequency control signals and takes them as input commands of gyro frame and magnetic suspension rotor, respectively. The semi-physical simulation results testify that the proposed method has good vibration suppression effect as well as improves the attitude convergence rate.

机译：本文通过利用磁悬浮控制和敏感陀螺仪的磁悬浮转子偏转，实现了航天器姿态和微振动的同步控制。设计扰动观察者以估计难以测量的复杂微振动，并且设计为集成控制器的自适应稳健滑模控制器，并且通过Lyapunov稳定性标准证明了其稳定性。引入带通滤波器以分别为低频和高频控制信号，并分别作为陀螺框架和磁悬浮转子的输入命令。半物理仿真结果证明了所提出的方法具有良好的振动抑制效果以及提高姿态会聚速率。

著录项

来源
《Proceedings of the Institution of Mechanical Engineers》 |2020年第15期|2197-2210|共14页
作者
Yuan Ren; Xiaocen Chen; Yuanwen Cai; Weijie Wang; Qiang Liu;
展开▼
作者单位

Department of Astronautics Science and Technology Space Engineering University;

Department of Astronautics Science and Technology Space Engineering University|Beijing Institute of Special Electromechanical Technology;

Department of Astronautics Science and Technology Space Engineering University;

Department of Astronautics Science and Technology Space Engineering University;

Beijing Institute of Petrochemical Technology;

展开▼
收录信息
原文格式 PDF
正文语种 eng
中图分类
关键词
Simultaneous control; attitude and micro-vibration; magnetically suspended control and sensitive gyroscope; disturbance observer; adaptive robust sliding mode control;

机译：同时控制;姿态和微振动;磁悬浮控制和敏感陀螺;干扰观察者;自适应鲁棒滑动模式控制;

相似文献

外文文献
中文文献
专利

1. Robust attitude control of nano-satellite using control moment gyros based on higher order sliding modes [J] . Ting Hao, Saburo Matunaga International Journal of Space Science and Engineering . 2014,第3期

机译：基于高阶滑模的控制力矩陀螺仪对纳米卫星的鲁棒姿态控制
2. Attitude tracking control for spacecraft with robust adaptive RBFNN augmenting sliding mode control [J] . Zou Yao Aerospace science and technology . 2016,第sepa期

机译：具有鲁棒自适应RBFNN增强滑模控制的航天器姿态跟踪控制
3. Robust Adaptive Gain Higher Order Sliding Mode Observer Based Control-constrained Nonlinear Model Predictive Control for Spacecraft Formation Flying [J] . Ranjith Ravindranathan Nair, Laxmidhar Behera 自动化学报：英文版 . 2018,第001期

机译：基于鲁棒自适应增益高阶滑模观测器的编队飞行控制约束非线性模型预测控制
4. Quaternion Based Sliding Mode Attitude Controller for a Spacecraft with Control Moment Gyros [C] . S Durga Nair, P. S Lal Priya, Arjun Narayanan International Workshop on Variable Structure Systems . 2018

机译：具有控制矩陀螺的航天器基于四元数的滑模姿态控制器
5. Nonlinear observer/controller designs for spacecraft attitude control systems with uncalibrated gyros. [D] . Thienel, Julie K. 2004

机译：具有未校准陀螺仪的航天器姿态控制系统的非线性观察器/控制器设计。
6. Performance Testing of a Magnetically Suspended Double Gimbal Control Moment Gyro Based on the Single Axis Air Bearing Table [O] . Peiling Cui, Huijuan Zhang, Ning Yan, 2012

机译：基于单轴空气轴承表的磁悬浮双云台控制力矩陀螺的性能测试
7. Robustness and Actuator Bandwidth of MRP-Based Sliding Mode Control for Spacecraft Attitude Control Problems [O] . Jung-Hoon Keum, Sung-Woong Ra 2009

机译：基于mRp的航天器姿态控制问题滑模控制的鲁棒性和执行器带宽
8. Nonlinear Decoupling Sliding Mode Control and Attitude Control of Spacecraft. [R] . Nartker, T. A., Singh, S. N., Iyer, A. 1989

机译：航天器非线性解耦滑模控制与姿态控制。

Adaptive robust sliding mode simultaneous control of spacecraft attitude and micro-vibration based on magnetically suspended control and sensitive gyro

摘要

著录项

相似文献

相关主题

期刊订阅