中国空间科学技术

Chinese Space Science and Technology

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The Research of Simulation Method of Dynamic Flux of Spacecraft by Infrared Heating Cage

Jia Yang (Beijing Institute of Spacecraft Environment Engineering,Beijing 100029) Xu Li Liu Qiang Jia Hong (Institute of Spacecraft System Engineering,Bijing 100086)   

  • Online:2001-04-25

Abstract: The dynamic mathematical model of infrared heating cage and flux sensor is founded by theory analysis,simulation research and experiment research in the engineering apply background of thermal balance test of some spacecraft.On the base of the model,the technique of simulation of dynamic flux of spacecraft in orbit is discussed,using infrared heating cage as flux simulation unit and adiabatic flux sensor as measure unit.