SATELLITE HAVING ASYMMETRIC SOLAR CELL PANEL SHAPE HAVING ASYMMETRIC PYRAMIDAL WHEEL STRUCTURE

摘要

The present invention relates to a satellite and, more specifically, to a satellite having solar cell panels asymmetrically arranged therein, the satellite comprising four wheels arranged in a pyramidal shape and having a wheel arrangement structure wherein the wheels are arranged at an angle preventing a zero speed switch problem from arising even though one wheel breaks down. Thus, it is possible to operate the satellite in a single direction without increasing the number of wheels, thereby preventing internal disturbance and ensuring price competitiveness.