Optimisation of the temperature control system of a geodetic space complex satellite

Abstract

A frequency generator is used to measure the signal delay between two surveying space objects. Thermostatting allows an increased level of stability. The temperature control system is the main thermal mode support system onboard. The mathematical model of this system is considered in this article. The analysis of factors influencing on Earth Satellite Vehicle is carried out. The variant of protection against kinetic influences is offered.