Solar cell array control strategy method suitable for yaw maneuvering satellite

The invention provides a solar cell array control strategy method suitable for a yaw maneuvering satellite. The method comprises the steps that the light condition of an orbit where the satellite is located is obtained; a satellite yaw maneuvering scheme is determined according to the light condition; and a solar cell array control strategy is obtained according to the satellite yaw maneuvering scheme. The problem of energy of on-orbit flying of the inclined orbit satellite is solved.