Error Mensuration of Temperature Coefficient between Formation Flying Small Satellites TT&C Equipment

The precise mensuration is needed between the formation flying small satellites, where temperature change results in error measurement. It is a hard problem to compensate the error caused by temperature change. In this paper, we propose a new error mensuration method for the temperature coefficient, which can implement the mensuration of temperature coefficient under the observe noise. This will help to the precise compensation of mensuration and synchronization. The simulation results show that the proposed algorithm can achieve the measurement of the temperature coefficient on satellites.