Space-Borne Integrated Design Analysis of Remote Sensing Camera on Geosynchronous Orbit

This Paper presents a space-borne integrated design analysis of remote sensing camera on Geosynchronous orbit. Considering the engineering practice, a typical structure forming method is given out which is applied to the Geosynchronous remote sensor camera. The organic unity of the integral work of satellite platform and the payload provides the steady support of the equipment, in addition, the difficulties of camera structure design are reduced remarkably. Simultaneously, the full consideration is given on the integration design of camera's thermal control structure and the satellite structure. As a result, the integrated design makes the less technical difficulties of the design and installation of thermal control structure, higher efficiency of passive thermal dissipation and less on-orbit power waste. Integrated design result shows, the payload had outstanding characteristics of high rigidity and high stability. Consequently, it successfully passed the qualification level of vibration test and thermal vacuum test. This paper details an integrated design method of space-borne remote sensing camera for further reference.