Martens, B., & Martinez, P. (2020). A fluid loop actuator for active spacecraft attitude control - A Parametric Sizing Model and the Design, Verification,
Validation and Test with a Prototype on an Air Bearing. Department of Electrical Engineering.
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Chicago Style (17th ed.) Citation
Martens, Bas, and Peter Martinez. A Fluid Loop Actuator for Active Spacecraft Attitude Control - A Parametric Sizing Model and the Design, Verification,
Validation and Test with a Prototype on an Air Bearing. Department of Electrical Engineering, 2020.
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MLA (9th ed.) Citation
Martens, Bas, and Peter Martinez. A Fluid Loop Actuator for Active Spacecraft Attitude Control - A Parametric Sizing Model and the Design, Verification,
Validation and Test with a Prototype on an Air Bearing. Department of Electrical Engineering, 2020.
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Warning: These citations may not always be 100% accurate.