Design and validation of an adaptive CubeSat transmitter system-Reference-Cited by-同舟云学术

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Design and validation of an adaptive CubeSat transmitter system

Published:2019-08 Issue: Volume:108 Page:118-126
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:

Jaswar Fitri,Al-Samman Ahmed M.,Abdul Rahman Tharek,Ahmad Yasser Asrul

Publisher

Elsevier BV

Subject

Electrical and Electronic Engineering

Reference29 articles.

1. NASA. Small spacecraft technology state of the art. 2014;(February):1–197.

2. CubeSat N, Initiative L. CubeSat 101: Basic concepts and processes for first-time CubeSat developers. 2017;(October).

3. The Cubesat Program. 6U CubeSat Design Specification Rev. PROVISIONAL. Calif. Polytech. State Univ. 2016;Rev. Provisional:26.

4. Cubesat radios: from kilobits to megabits;Klofas;Gr Syst Archit Work,2014

5. Space mission analysis and design;Wertz,1991

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1. Design and analysis of a nanosatellite attitude control system using processor-in-the-loop approach;AEU - International Journal of Electronics and Communications;2023-11

2. E-design and manufacturing approach for Cubesat solar panel deployment mechanism;International Journal on Interactive Design and Manufacturing (IJIDeM);2022-03-15

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