Optimum spacecraft attitude control methods for a combined attitude and thermal control system

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Optimum spacecraft attitude control methods for a combined attitude and thermal control system

Spacecraft missions need efficient and precise attitude control systems. With the aim of reducing the vehicle volume and mass, and for a greater reliability, a system combining the conventional spacecraft attitude control and thermal control systems in a single system is proposed. The combined attit...

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Bibliographic Details
Main Author:	Al-Khodari, M. Saleh Basha
Format:	Thesis
Language:	English
Published:	2011
Subjects:	Space vehicles
Online Access:	http://psasir.upm.edu.my/id/eprint/41781/ http://psasir.upm.edu.my/id/eprint/41781/1/FK%202011%206R.pdf

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