What is it about?
The paper proposes a conceptual CubeSat design that uses a single thruster and a single Variable Speed Control Moment Gyro. In this analysis it is shown that such a spacecraft could potentially be developed and used for rendezvous missions.
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This page is a summary of: Control of a Thrust-Vectoring CubeSat Using a Single Variable-Speed Control Moment Gyroscope, Journal of Guidance Control and Dynamics, October 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g005181.
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