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...

पूर्ण विवरण

ग्रंथसूची विवरण
मुख्य लेखक: Chak, Yew Chung
स्वरूप: थीसिस
भाषा:अंग्रेज़ी
प्रकाशित: 2019
विषय:
ऑनलाइन पहुंच:http://psasir.upm.edu.my/id/eprint/84366/1/FK%202019%20118%20-%20ir.pdf

समान संसाधन