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Jinaykumar Patel

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Open access Sep 2026

Optimal Thruster Layout Design and Closed-Loop 6DOF Evaluation for Small Satellites

A systematic approach for the design and evaluation of thruster layouts allowing six-degrees-of-freedom (6-DOF) control of small cube satellites for rendezvous and proximity operations is introduced. Initiating from a symmetric 24-thruster layout, all feasible configurations are enumerated and assessed using a controll...

Suguru Sato, Jinaykumar Patel, K. Subbarao · 0 citations

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