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本文给出了太阳同步兼回归轨道的一种控制方法,并提出用偏置半长轴补偿倾角误差引起的地面轨迹漂移。在轨道保持中采用了超调模式。 该方法适用于地球观测卫星的普遍情况,并可用于这类卫星的轨道设计。
In this paper, a control method of solar synchronization and return orbit is given, and the drift of the ground track caused by compensating the tilt error by offsetting the semi-major axis is proposed. Overshoot mode is used in orbit hold. The method is applicable to the general situation of Earth observation satellites and can be used for the orbital design of such satellites.