A novel design of spacecraft combined attitude & sun tracking system using a versatile fuzzy controller-Reference-Cited by-同舟云学术

A novel design of spacecraft combined attitude & sun tracking system using a versatile fuzzy controller

Published:2015-10-05 Issue:6 Volume:87 Page:530-539
ISSN:0002-2667
Container-title:Aircraft Engineering and Aerospace Technology
language:en
Short-container-title:Aircraft Eng & Aerospace Tech

Author:

Chak Yew-Chung,Varatharajoo Renuganth

Publisher

Emerald

Reference7 articles.

1. Allaudin, M.F. and Varatharajoo, R. (2011), “Spacecraft combined attitude and sun tracking system”,Mathematics in Engineering, Science and Aerospace, Vol. 2 No. 4, pp. 413-421.

2. Control of longitudinal movement of a plane using combined model reference adaptive control

3. Fuzzy control for a non-linear MIMO plant subject to control constraints

4. Onboard errors of the combined energy and attitude control system

5. Operation for the combined energy and attitude control system

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