Attitude And Orbit Coupling
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1. Análise do acoplamento entre o controle de atitude e de trajetória durante manobras orbitais de empuxo contínuo / Coupling analysis between attitude control and orbital maneuvering trajectory during continuous thrust
This work considers the coupling between attitude and orbit control used during an orbital transference which uses a continuous propulsive system capable impulse for a long time. The dynamic equations of movement are used to propagate the orbit and attitude states. It is studied some cases which comes from the effect of control during the orbital transferenc
Publicado em: 2010