Quaternion Based Sliding Mode Attitude Controller for a Spacecraft with Control Moment Gyros
Author:
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/8428393/8460209/08460457.pdf?arnumber=8460457
Cited by 4 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. Logic-based gimbal compensator for the double-gimbal scissored-pair control moment gyroscope using magnetic torquers;Advances in Space Research;2024-01
2. Constraints-Aware Trajectory Tracking Control of Spacecraft Attitude using LPV and MPC;2023 27th International Conference on Methods and Models in Automation and Robotics (MMAR);2023-08-22
3. Design of Sliding Mode Techniques for a CMG-based Testbed Attitude Control System;IFAC-PapersOnLine;2021
4. Robust trajectory tracking control of an underactuated control moment gyroscope via neural network–based feedback linearization;Neurocomputing;2020-08
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