A combined attitude and sun tracking system for spacecraft using fuzzy logic control

Many spacecraft attitude control systems today use reaction wheels to deliver precise torques to achieve a three-axis attitude stabilization. Despite the extensive studies in attitude controllers, failures still can occur in a spacecraft system. For example, if a spacec...

Full description

Saved in:
Bibliographic Details
Main Author: Chak, Yew Chung
Format: Thesis
Published: 2019
Online Access:http://psasir.upm.edu.my/id/eprint/84366/1/FK%202019%20118%20-%20ir.pdf
Tags: Add Tag
No Tags, Be the first to tag this record!