| Citation: | LU P，ZHAO Z M，GAO T，et al. Thermal control design and verification for high resolution stereo mapping camera system[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（4）：768-779 （in Chinese） doi: 10.13700/j.bh.1001-5965.2022.0854
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The temperature stability of optical system and detector of high precision stereo mapping camera affects the mapping accuracy of mapping camera. For transmission optical system, multi-stage external heat flow suppression technology is adopted to improve the temperature stability of the star camera lens by 6 times; for reflective optical system, thermal control technologies such as indirect radiation temperature control are adopted to make the temperature stability of the primary and secondary mirrors reach ±0.3 ℃; for high-power charge-coupled device (CCD), energy-saving temperature control technology based on loop heat pipe (LHP) is adopted to make the LHP driving power cycle average from 60 W to 33.8 W, while saving about 40% of the primary condenser area and mass; for CMOS, using two-stage temperature fluctuation suppression technology, the temperature stability is ±0.3 ℃. The method of ground thermal test was investigated, and the flight temperature data of key components of the mapping camera system under extreme space environment were reported, which fully verified the correctness of the thermal control design method.
| [1] |
黎明, 吴清文, 江帆, 等. 三线阵立体测绘相机热控系统的设计[J]. 光学精密工程, 2010, 18(6): 1367-1373.
LI M, WU Q W, JIANG F, et a1. Design of thermal control system for three-linear array mapping cameras[J]. Optics and Precision Engineering, 2010, 18(6): 1367-1373(in Chinese).
|
| [2] |
胡莘, 曹喜滨. 三线阵立体测绘卫星的测绘精度分析[J]. 哈尔滨工业大学学报, 2008, 40(5): 695-699.
HU X, CAO X B. Analysis on precision of stereo mapping microsatellite using three-line array CCD images[J]. Journal of Harbin Institute of Technology, 2008, 40(5): 695-699(in Chinese).
|
| [3] |
曹海翊, 刘付强, 赵晨光, 等. 高分辨率立体测绘卫星技术研究[J]. 遥感学报, 2021, 25(7): 1400-1410.
CAO H Y, LIU F Q, ZHAO C G, et a1. The study of high resolution stereo mapping satellite[J]. National Remote Sensing Bulletin, 2021, 25(7): 1400-1410(in Chinese).
|
| [4] |
赵振明, 孟庆亮, 张焕冬, 等. CCD器件用机械泵驱动两相流体回路仿真与试验[J]. 北京航空航天大学学报, 2019, 45(5): 893-901. doi: 10.13700/j.bh.1001-5965.2018.0519
ZHAO Z M, MENG Q L, ZHANG H D, et al. Simulation and experimental study of mechanically pumped two-phase loop for CCD[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(5): 893-901(in Chinese). doi: 10.13700/j.bh.1001-5965.2018.0519
|
| [5] |
CHOI M K. Thermal design to meet stringent temperature gradient/stability requirements of SWIFT BAT detectors: AIAA-2000-2905[R]. Reston: AIAA, 2000.
|
| [6] |
HOANG T T, O’CONNELL T A, KU J, et al. Large area cryocooling for far infrared telescope[C]//Proceedings Volume 5172-Cryogenic Optical Systems and Instruments X. Bellingham: SPIE, 2003, 5172: 77-85.
|
| [7] |
黄金印, 潘福明, 傅伟纯, 等. 高分七号卫星激光测高仪热设计及验证[J]. 航天器工程, 2020, 29(3): 138-143.
HUANG J Y, PAN F M, FU W C, et al. Thermal design and verification of laser altimeter for GF-7 satellite[J]. Spacecraft Engineering, 2020, 29(3): 138-143(in Chinese).
|
| [8] |
杨涛, 赵石磊, 高腾, 等. 航天分散热源控温用环路热管设计及飞行应用[J]. 宇航学报, 2021, 42(6): 798-806.
YANG T, ZHAO S L, GAO T, et al. Design and in-orbit application of temperature controlled loop heat pipe for aerospace distributed heat sources[J]. Journal of Astronautics, 2021, 42(6): 798-806(in Chinese).
|
| [9] |
杨昌鹏, 赵欣, 辛强. 倾斜轨道星敏感器热控设计及在轨分析[J]. 航天器工程, 2013, 22(6): 59-64.
YANG C P, ZHAO X, XIN Q. Thermal design and on-orbit thermal analysis on star sensor of inclined-orbit satellite[J]. Spacecraft Engineering, 2013, 22(6): 59-64(in Chinese).
|
| [10] |
江帆, 王忠素, 陈立恒, 等. 星敏感器组件的热设计[J]. 红外与激光工程, 2014, 43(11): 3740-3745. doi: 10.3969/j.issn.1007-2276.2014.11.041
JIANG F, WANG Z S, CHEN L H, et al. Thermal design of star sensor assembly[J]. Infrared and Laser Engineering, 2014, 43(11): 3740-3745(in Chinese). doi: 10.3969/j.issn.1007-2276.2014.11.041
|
| [11] |
孙鹏, 魏然, 赵欣, 等. 分体式主动像元星敏感器高温度稳定度热设计及在轨验证[J]. 航天器环境工程, 2019, 36(4): 380-386.
SUN P, WEI R, ZHAO X, et al. High temperature-stability thermal design of separated type aps star sensor and the on-orbit test[J]. Spacecraft Environment Engineering, 2019, 36(4): 380-386(in Chinese).
|
| [12] |
王伟之, 王妍, 于艳波, 等. 亚角秒级星相机的精度测定[J]. 红外与激光工程, 2018, 47(9): 1605-1609.
WANG W Z, WANG Y, YU Y B, et a1. Accuracy determination for sub-arcsec star camera[J]. Infrared and Laser Engineering, 2018, 47(9): 1605-1609(in Chinese).
|
| [13] |
贾永丹, 王伟之, 孙建, 等. 高精度星相机光学系统像质评价及实现[J]. 空间控制技术与应用, 2018, 44(3): 897-906.
JIA Y D, WANG W Z, SUN J, et a1. Evaluation and implementation of image quality in high-precision star camera optical system[J]. Aerospace Control and Application, 2018, 44(3): 897-906(in Chinese).
|
| [14] |
邓永涛, 李旭, 颜凡江. 一种星载激光测距仪姿态的确定方法及误差分析[J]. 航天返回与遥感, 2015, 36(3): 86-91. doi: 10.3969/j.issn.1009-8518.2015.03.012
DENG Y T, LI X, YAN F J. Attitude determination method and error analysis of spaceborne laser range finder[J]. Spacecraft Recovery & Remote Sensing, 2015, 36(3): 86-91(in Chinese). doi: 10.3969/j.issn.1009-8518.2015.03.012
|
| [15] |
孟恒辉, 耿利寅, 李国强. 激光通信器热设计与热试验[J]. 红外与激光工程, 2014, 43(7): 2295-2299.
MENG H H, GENG L Y, LI G Q. Thermal control design and experiment for laser communication equipment[J]. Infrared and Laser Engineering, 2014, 43(7): 2295-2299(in Chinese).
|
| [16] |
高腾, 杨涛, 赵石磊, 等. 环路热管在低温真空环境下的控温性能试验研究[J]. 航天返回与遥感, 2019, 40(4): 38-47.
GAO T, YANG T, ZHAO S L, et al. Experimental research on temperature controlling performance of loop heat pipe in vacuum and low temperature environment[J]. Spacecraft Recovery & Remote Sensing, 2019, 40(4): 38-47(in Chinese).
|
| [17] |
KU J. Operating characteristics of loop heat pipes[C]//29th International Conference on Environmental System, 1999: 1-17.
|
| [18] |
KAYA T, HOANG T T. Mathematical modeling of loop heat pipes and experimental validation[J]. Journal of Thermophysics and Heat Transfer, 1999, 13(3): 314-320. doi: 10.2514/2.6461
|
| [19] |
MAYDANIK Y F. Loop heat pipes[J]. Applied Thermal Engineering, 2005, 25(5-6): 635-657. doi: 10.1016/j.applthermaleng.2004.07.010
|
| [20] |
MAJDANIK Y G, FERSHTATER Y G, PASTUKTOV V G, et al. Thermoregulation of loops with capillary pumping for space use[C]//22nd International Conference on Environmental Systems, 1992: 921169.
|
| [21] |
LAUNAY S, SARTRE V, BONJOUR J. Parametric analysis of loop heat pipe operation: A literature review[J]. International Journal of Thermal Sciences, 2007, 46(7): 621-636. doi: 10.1016/j.ijthermalsci.2006.11.007
|
| [22] |
沈维道, 蒋智敏, 童钧耕. 工程热力学[M]. 3版. 北京: 高等教育出版社, 2006: 205.
SHEN W D, JIANG Z M, TONG J G. Engineering thermodynamics[M]. 3rd ed. Beijing: Higher Education Press, 2006: 205(in Chinese) .
|
| [23] |
柏立战, 林贵平, 张红星. 环路热管稳态建模及运行特性分析[J]. 北京航空航天大学学报, 2006, 32(8): 894-898.
BAI L Z, LIN G P, ZHANG H X. Steady state modeling of loop heat pipes and operating characteristics analysis[J]. Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(8): 894-898(in Chinese).
|
| [24] |
宋欣阳, 高娟, 赵振明, 等. 间接热控在高分辨率光学遥感器恒温控制中的应用[J]. 航天返回与遥感, 2015, 36(2): 46-52.
SONG X Y, GAO J, ZHAO Z M, et a1. Application of indirect thermal control technology for constant temperature control of HR optical remote sensor[J]. Spacecraft Recovery & Remote Sensing, 2015, 36(2): 46-52(in Chinese).
|
| [25] |
张超, 邢辉, 宋俊儒, 等. 大口径凹椭球面反射镜光轴偏心测量方法[J]. 红外与激光工程, 2021, 50(12): 386-392.
ZHANG C, XING H, SONG J R, et al. Measurement of optical axis eccentricity of a large-aperture concave ellipsoid mirror[J]. Infrared and Laser Engineering, 2021, 50(12): 386-392 (in Chinese).
|
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