Nonlinear Attitude Control of Flexible Spacecraft With Scissored Pairs of Control Moment Gyros-Reference-Cited by-同舟云学术

Nonlinear Attitude Control of Flexible Spacecraft With Scissored Pairs of Control Moment Gyros

Published:2012-06-05 Issue:5 Volume:134 Page:
ISSN:0022-0434
Container-title:Journal of Dynamic Systems, Measurement, and Control
language:en
Short-container-title:

Author:

Fan Jixiang¹,Zhou Di²

Affiliation:

1. Department of Control Science and Engineering, Harbin Institute of Technology, Mailbox327, Harbin, China; Department of Electronic Engineering, Harbin Normal University, Harbin, China

2. Department of Control Science and Engineering, Harbin Institute of Technology, Mailbox327, Harbin, China

Abstract

Dynamic equations describing the attitude motion of flexible spacecraft with scissored pairs of control moment gyroscopes are established. A nonlinear controller is designed to drive the flexible spacecraft to implement three-axis large-angle attitude maneuvers with the vibration suppression. Singularity analysis for three orthogonally mounted scissored pairs of control moment gyros shows that there exists no internal singularity in this configuration. A new pseudo-inverse steering law is designed based on the synchronization of gimbal angles of the twin gyros in each pair. To improve the synchronization performance, an adaptive nonlinear feedback controller is designed for each pairs of control moment gyros by using the stability theory of Lyapunov. Simulation results are provided to show the validity of the controllers and the steering law.

Publisher

ASME International

Subject

Computer Science Applications,Mechanical Engineering,Instrumentation,Information Systems,Control and Systems Engineering

Link

http://asmedigitalcollection.asme.org/dynamicsystems/article-pdf/doi/10.1115/1.4006368/5785172/054502_1.pdf

Reference12 articles.

1. Preferred Gimbal Angles for Single Gimbal Control Moment Gyros;Vadali;J. Guid. Control Dyn.

2. Precision Spacecraft Pointing Using Single-Gimbal Control Moment Gyros With Disturbance;Heiberg;J. Guid. Control Dyn.

3. Singular Direction Avoidance Steering for Control Moment Gyros;Ford;J. Guid. Control Dyn.

4. Singularity Robust Steering Logic for Redundant Single-Gimbal Control Moment Gyros;Wie;J. Guid. Control Dyn.

5. Singularity Analysis and Visualization for Single-Gimbal Control Moment Gyro Systems;Wie;J. Guid. Control Dyn.

Cited by 7 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Composite Control of Attitude Tracking and Vibration Suppression of a Rigid–Flexible Coupled System;Journal of Aerospace Engineering;2021-07

2. Model predictive steering control law for double gimbal scissored-pair control moment gyros;Acta Astronautica;2021-06

3. Steering control law for double-gimbal scissored-pair CMG;Advances in Space Research;2020-08

4. Integrated control of attitude maneuver and vibration suppression of flexible spacecraft based on magnetically suspended control moment gyros;Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science;2020-07-22

5. Attitude control of reentry vehicles in roll channel using single-gimbal control moment gyros and a reaction control system;Advances in Mechanical Engineering;2017-11