[1]HOWARD E. NOAA’s future GOES satellite program[C]//GOES8 and Beyond Proceeding SPIE. Washington. D.C.: SPIE, 1996.
[2]HAILE W. GOESR preliminary jitter analysis[J]. Swales Aerospace. 2002, 3: 2029.
[3]MAX E N, JON F L. MONOLITHIC V. Deployable primary mirror trade considerations for the next generation space telescope[C]//Advanced Telescope Design, Fabrication and Control. SPIE, 2002.
[4]DANIEL R C, DAVID N J. Technology for the next generation space telescope[J]. SPIE, 2000(4013): 784794
[5]BILIMORIA K D, WEI B. Timeoptimal threeaxis reorientation of a rigid spacecraft[J]. Journal of Guidance, Control, and Dynamics, 1993, 16: 446452.
[6]SCRIVENER S, THOMPSON R. Survey of time optimal attitude maneuvers[J]. Journal of Guidance, Control, and Dynamics, 1994, 17(2): 225233.
[7]BYERS R M, VADALI S R, JUNKINS J L, Nearminimum time, closedloopslewing of flexible spacecraft[J]. Journal of Guidance,Control,and Dynamics, 1990, 13(1): 5765.
[8]LI Y. Modeling and control of a flexible spacecraft for largeangle rapid maneuvers[J]. Automatic control in Aerospace, 1998: 341346.
[9]刘林, 王彦荣. 卫星轨道预报的一种分析方法[J]. 天文学报, 2005, 46(3): 307313.
LIU L, WANG Y R. An analytical method for satellite orbit forecasting[J]. Acta Astronomica Sinica., 2005, 46(3): 307313.
[10]彭洲, 李振松, 乔国栋, 等. 地球静止轨道遥感卫星相机太阳规避设计[J]. 中国空间科学技术, 2015, 35(2): 5762.
PENG Z, LI Z S, QIAO G D, et al. Sunlight avoidance design for camera of geostationary orbit remote sensing satellite[J]. Chinese Space Science and Technology, 2015, 35(2): 5762. |