Satellite Adaptive Attitude Control Based on Decentralized Minimal Control in the Presence of Reaction wheel Accurate Model

In this paper, an adaptive controller based on decentralized minimal control synthesis is designed n order to control an attitude of specific remote sensing satellite. The main design purposes are performing spinning, three axis and large angle maneuver as well as achieving a stable system and track...

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Bibliographic Details

Published in:	فصلنامه علوم و فناوری فضایی
Main Authors:	Ali Mehrabi, Fathallah Ommi
Format:	Article
Language:	Persian
Published:	Aerospace Research Institute 2016-05-01
Subjects:	adaptive attitude control reaction wheel model satellite uncertainty and actuator saturation
Online Access:	https://jsst.ias.ir/article_34183_1777a2f10ca748b64900eab5ad5a489f.pdf