A Magnetometer-Only Attitude Determination Strategy for Small Satellites: Design of the Algorithm and Hardware-in-the-Loop Testing

Attitude determination represents a fundamental task for spacecraft. Achieving this task on small satellites, and nanosatellites in particular, is further challenging, because the limited power and computational resources available on-board, together with the low development budget, set strict const...

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Bibliographic Details
Main Authors: Stefano Carletta, Paolo Teofilatto, M. Salim Farissi
Format: Article
Language:English
Published: MDPI AG 2020-01-01
Series:Aerospace
Subjects:
hil
Online Access:https://www.mdpi.com/2226-4310/7/1/3

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