Attitude determination and control of LEO microsatellites

The Attitude Determination and Control System algorithm and code have been developed and tested for the possible use in the proposed X-Sat, a LEO microsatellite of NTU. The X-Sat is currently under development and is expected to be launched in 2005 into a circular orbit at a height of 800km. An Equa...

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Bibliographic Details
Main Author: Wee, Melisa Toon Cheng.
Other Authors: Arichandran, K.
Format: Theses and Dissertations
Published: 2008
Subjects:
Online Access:http://hdl.handle.net/10356/3724
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Institution: Nanyang Technological University
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