Design and analysis of a nanosatellite attitude control system using processor-in-the-loop approach-Reference-Cited by-同舟云学术

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Design and analysis of a nanosatellite attitude control system using processor-in-the-loop approach

Published:2023-11 Issue: Volume:171 Page:154880
ISSN:1434-8411
Container-title:AEU - International Journal of Electronics and Communications
language:en
Short-container-title:AEU - International Journal of Electronics and Communications

Author:

El Fatimi Aziz^ORCID,Addaim Adnane,Guennoun Zouhair

Publisher

Elsevier BV

Subject

Electrical and Electronic Engineering

Reference39 articles.

1. CubeSat missions and applications;Cappelletti,2021

2. Design and validation of an adaptive CubeSat transmitter system;Jaswar;AEU - Int J Electron Commun,2019

3. Low earth orbit satellite design;Sebestyen,2018

4. Satellite positioning and navigation: Fundamentals, operation and application of global navigation satellite systems;Finger;AEU - Int J Electron Commun,2010

5. Feasibility assessment of passive stabilisation for a nanosatellite with aeroshell deployed by orbit-attitude-aerodynamics simulation platform;Berthet;Acta Astronaut,2020

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