Simulation of thermal control system of nano satellite based on fuzzy control

[1] 徐济万．小卫星应用与热控系统研究[M]．上海:上海卫星工程研究所,2002:130-140 Xu Jiwan．Micosatellite application and thermal control system research[M]．Shanghai:Shanghai Satellite Project Research Institute,2002:130-140(in Chinese) [2] Butcher M R.Spacecraft thermal design:particular problems with small satellites[J]．Journal of Aerospace Engineering,1999,213(4):245-253 [3] Volodymyr B. Microsatellite thermal control—concepts and components[J]．Acta Astronautica, 2005,56(1-2):161-170 [4] 闵桂荣,郭舜．航天器热控制[M]．北京:科学出版社,1998:420-428 Min Guirong,Guo Xun．Areospacecraft thermal control[M]．Beijing Science Press,1998:420-428(in Chinese) [5] 李运泽．卫星热热平衡试验的温度预测与仿真模型[J]．北京航空航天大学学报,2004,30(9):882-884 Li Yunze．Temperature prediction and simulation model of satellite’s thermal balance test[J]．Journal of Beijing University of Astronautics and Astronautics,2004,30(9):882-884 (in Chinese) [6] 李运泽．卫星热控系统的动态特性建模与仿真[J]．北京航空航天大学学报,2005,31(3):372-374 Li Yunze．Dynamical modeling and simulation of satellite thermal control system[J]．Journal of Beijing University of Astronautics and Astronautics,2005,31(3):372-374 (in Chinese)