Fault tolerant control for spacecraft attitude control systems

Future spacecraft are expected to achieve highly accurate pointing, fast slewing from large initial condition, and reliable maneuvers in the presence of environmental disturbances, unknown or uncertain inertia parameters, control input saturation, and component failures. Actuators play an important...

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Bibliographic Details
Main Author: Shen, Qiang
Other Authors: Poh Eng Kee
Format: Theses and Dissertations
Language:English
Published: 2016
Subjects:
Online Access:https://hdl.handle.net/10356/69067
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Institution: Nanyang Technological University
Language: English
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