Comparative Analysis of Low Earth Orbit Satellite Attitude Determination using Sensor Integration and Attitude Estimation using Kalman Filter

The objective of the research is to undergo a performance comparison in terms of accuracy, convergence time, amount of memory, etc. between the satellite attitude determination and attitude estimation using non-linear filters. The fundamental approach towards it is to design an OBC (On Board Compute...

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Bibliographic Details
Main Author: M. RAJA
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2021-06-01
Series:INCAS Bulletin
Subjects:
Online Access:https://bulletin.incas.ro/files/raja-m__vol_13_iss_2.pdf