The development and performance evaluation of Particle Filter–H∞ Filter for attitude estimation of a small satellite in low earth orbit

The accurate determination of the attitude of small satellites is essential for missions with stringent pointing requirements. Small satellites such as CubeSats are subject to mass and volume constraints, which directly affects their ability to carry more extensive and demanding payloads and limits...

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Bibliographic Details
Main Author: Aman, Asma Mohammad Nusrat
Format: Thesis (University of Nottingham only)
Language:English
Published: 2023
Subjects:
Online Access:https://eprints.nottingham.ac.uk/73605/