An event-trigger control scheme for spacecraft attitude control

This report discussed on the proposal of event-trigger control design scheme for spacecraft attitude stabilization problem to reduce communication burden between spacecraft attitude controller and actuator. Both controller and event-trigger controller are designed simultaneously in order to compensa...

Повний опис

Бібліографічні деталі
Автор: Leong, Wei Yang
Інші автори: Wen Changyun
Формат: Final Year Project (FYP)
Мова:English
Опубліковано: 2017
Предмети:
Онлайн доступ:http://hdl.handle.net/10356/71837