Tilted wheel satellite attitude control with air-bearing table experimental results-Reference-Cited by-同舟云学术

Tilted wheel satellite attitude control with air-bearing table experimental results

Published:2015-12 Issue: Volume:117 Page:414-429
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Inumoh Lawrence O.^ORCID,Forshaw Jason L.,Horri Nadjim M.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference16 articles.

1. The Bendix Corp., Control Moment Gyroscope Gimbal Actuator Study, Technical Report AFFDRL-TR-66-158, 210p, The Bendix Corporation, November 1966.

2. Inverse kinematic solutions with singularity robustness for redundant manipulator control;Nakamura;ASME J. Dyn. Syst. Meas. Control,1986

3. Rapid multitarget acquisition and pointing control of agile spacecraft;Wie;AIAA J. Guidance Control Dyn.,2002

4. Feedback control law for variable speed control moment gyros;Schaub;J. Astronaut. Sci.,1998

5. V.J. Lappas, A control moment gyro (CMG) based attitude control system (ACS) for agile small satellites (Ph.D. thesis), Surrey Space Centre, University of Surrey, October 2002.

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. Attitude control for spacecraft using pyramid-type variable-speed control moment gyros;Acta Astronautica;2020-08

2. Extended validation of a ground-based three-axis spacecraft simulator model;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2020-07-13

3. Globally asymptotic three-axis attitude control for a two-wheeled small satellite;Acta Astronautica;2019-04

4. Modeling of disturbance torque in an aerostatic bearings-based nano-satellite simulator;Journal of Systems Engineering and Electronics;2018

5. Mass properties identification and automatic mass balancing system for satellite attitude dynamics simulator;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2017-12-17