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COBEM 2017
24th ABCM International Congress of Mechanical Engineering
Revisiting the Dual-spin Spacecraft Dynamics during Plat-form Spin-up with Limited Torque Supply
Submission Author:
José Manoel Balthazar , SP , Brazil
Co-Authors:
Edson Cereja, Airton Nabarrete, Angelo Marcelo Tusset, Rodrigo Tumolin Rocha, Jorge Luis Palacios Felix, Reyolando Brasil, José Manoel Balthazar
Presenter: José Manoel Balthazar
doi://10.26678/ABCM.COBEM2017.COB17-0256
Abstract
This work comprises a review on the attitude dynamics of a gyrostat used as an idealized model for Dual Spin Satellites as well as the analysis of some control strategies aimed at overcoming resonance traps occurring during platform spinup, in particular considering maneuvers executed with limited power supply.
Keywords
dual spin satellite, attitude, control, non-ideal oscillations
