M. Yu. Ovchinnikov, Hao-Chi Chang, S. A. Mirer, S. S. Tkachev, D. S. Roldugin, “Dynamical model of a satellite with controllable solar array”, Keldysh Institute preprints, 2015,026, 19 pp.

Dynamical model of a satellite with controllable solar array

M. Yu. Ovchinnikov, Hao-Chi Chang, S. A. Mirer, S. S. Tkachev, D. S. Roldugin

Abstract: Satellite with 3DOF solar panel is considered. Satellite is a rigid body while solar panel consists of three parts connected by 1 DOF hinges. The work is aimed at the satellite-panel system attitude dynamical model construction.

Keywords: complex structure, solar panel, 3DOF hinge, equations of motion.

Language: English