Tabletop Testbed for Attitude Determination and Control of Nanosatellites

Author:

Silva Rodrigo Cardoso da1,Guimarães Fernando Cardoso2,Loiola João Victor Lopes de2,Borges Renato Alves3,Battistini Simone4,Cappelletti Chantal5

Affiliation:

1. Postgraduate Student, Dept. of Electrical Engineering, Univ. of Brasília, Campus Darcy Ribeiro, Brasília-DF CEP 70910-900, Brazil (corresponding author).

2. Postgraduate Student, Dept. of Electrical Engineering, Univ. of Brasília, Campus Darcy Ribeiro, Brasília-DF CEP 70910-900, Brazil.

3. Assistant Professor, Dept. of Electrical Engineering, Univ. of Brasília, Campus Darcy Ribeiro, Brasília-DF CEP 70910-900, Brazil.

4. Assistant Professor, Faculty of Gama, Univ. of Brasília, Campus Gama, Gama-DF CEP 72444-240, Brazil.

5. Assistant Professor, Dept. of Mechanical, Materials, and Manufacturing Engineering, Univ. of Nottingham, Nottingham NG7 2RD, UK.

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Reference21 articles.

1. Three-Axial Helmholtz Coil Design and Validation for Aerospace Applications

2. Brewer M. R. 2012. “CubeSat attitude determination and Helmholtz cage design.” M.S. thesis Dept. of Aeronautics and Astronautics Air Force Institute of Technology.

3. Carletta S. and P. Teofilatto. 2017. “Design and development of a full 5-DOF testbed for testing nanosatellites formation flying rendezvous and proximity operations.” In Proc. 9th Int. Workshop on Satellite Constellations and Formation Flying. Boulder CO: Univ. of Colorado Boulder.

4. Carrara V. and P. G. Milani. 2007. “Controle de uma mesa de mancal a ar de um eixo equipada com giroscópio e roda de reação.” In V SBEIN-Simpósio Brasileiro de Engenharia Inercial 26–29. Rio de Janeiro Brazil: Military Institute of Engineering.

5. Automatic Mass Balancing of a Spacecraft Three-Axis Simulator: Analysis and Experimentation

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