Design, Manufacturing, and Ground Testing of a Control-Moment Gyro for Agile Microsatellites-Reference-Cited by-同舟云学术

Design, Manufacturing, and Ground Testing of a Control-Moment Gyro for Agile Microsatellites

Published:2017-09 Issue:5 Volume:30 Page:04017039
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Arena Lorenzo¹,Piergentili Fabrizio²,Santoni Fabio³

Affiliation:

1. Ph.D. Student, DIMA-Dipartimento di Ingegneria Meccanica e Aerospaziale, Università di Roma La Sapienza, Via Eudossiana, 18, 00184 Roma, Italy (corresponding author).

2. Assistant Professor, DIMA-Dipartimento di Ingegneria Meccanica e Aerospaziale, Università di Roma La Sapienza, Via Eudossiana, 18, 00184 Roma, Italy.

3. Associate Professor, DIAEE-Dipartimento di Ingegneria Astronautica, Elettrica ed Energetica, Università di Roma La Sapienza, Via Eudossiana, 18, 00184 Roma, Italy.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000754

Reference21 articles.

1. Arena L. (2014). “A small low-cost and maintenance-free test-bed for agile satellite attitude control using momentum exchange devices.” Proc. 65th Int. Astronautical Congress Toronto.

2. Development experience of the attitude control system using single-axis control moment gyros for long-term orbiting space stations

3. Dynamics of a High-Agility, Low-Power Imaging Payload

4. Flight Performance of Skylab Attitude and Pointing Control System

5. Clark C. Worral K. and Yavuzoğlu E. (2010). “A control moment gyro for dynamic attitude control of small satellites.” Proc. 24th Annual AIAA/USU Conf. on Small Satellites Technical Session XI: Mission Enabling Technologies 2.

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