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Ultraviolet detection has advantages of high sensitivity and low false alarm rate. Analysis of ultraviolet characteristics has great significance for space target detection. An accurate modeling method is proposed for the ultraviolet characteristics of space target. Based on the background environment and material properties of space target, region and grid division are generated, and the mathematical model of ultraviolet characteristics of space target is established by introducing bidirectional reflectance distribution function. The position relations of target, detector and background radiation source are determined by coordinate transformation algorithm. The calculation flow for ultraviolet characteristics of space target is derived. Finally, the observed ranges and irradiation distributions of Ziyuan-1 and Fengyun-3 satellite are calculated by the given parameters. The simulation results demonstrate the validity of the modeling method.
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Keywords:
- space target /
- ultraviolet characteristics /
- bidirectional reflectance distribution function /
- modeling and simulation
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[31] [32] Yu J H, Su Z L 2006 J. Spacec. Telem. Track Comm. Technol. 25 52 ( in Chinese) [余建慧、苏增立 2006 飞行器测控学报25 52]
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[37] -
[1] Yao L X, Qiu W L, Wang F H 1995 Optical Characteristics of Target and Environment (Beijing: Aerospace Press) p1 ( in Chinese) [姚连兴、仇维礼、王福恒 1995 目标和环境的光学特性 ( 北京: 宇航出版社) 第1页]
[2] [3] Wang J J, Yu X H 2006 J. Acad. Equip. Comm. Technol. 17 33 ( in Chinese) [王杰娟、于小红 2006 装备指挥技术学院学报 17 33]
[4] [5] Joseph C L 1997 Proc. SPIE 2999 244
[6] [7] Cox R J, Strickland D J, Evans J S, Wright K C, Paxton L J 1994 Proc. SPIE 2282 261
[8] Mende S B, Fuselier S A 1993 Opt. Eng. 32 3139
[9] [10] [11] Zhou M, Zhao D G 2009 Acta Phys. Sin. 58 7255 ( in Chinese) [周 梅、赵德刚 2009 物理学报58 7255]
[12] [13] Zhou M, Zuo S H, Zhao D G 2007 Acta Phys. Sin. 56 5513 (in Chinese) [周 梅、左淑华、赵德刚 2007 物理学报56 5513]
[14] [15] Schuehle U H, Hochedez J E, Pau J L, Rivera C, Munoz E 2004 Proc. SPIE 5171 231
[16] [17] Wang H Y, Zhang W, Wang Z L 2009 J. Appl. Opt. 30 410 (in Chinese) [汪洪源、张 伟、王治乐 2009 应用光学 30 410]
[18] [19] Nicodemus F E 1965 Appl. Opt. 4 767
[20] Ye H X, Jin Y Q 2008 Acta Phys. Sin. 57 839 ( in Chinese) [叶红霞、金亚秋 2008 物理学报 57 839]
[21] [22] Xu L Q, Li H, Xiao Z Y 2008 Acta Phys. Sin. 57 6030 ( in Chinese) [徐兰青、李 晖、肖郑颖 2008 物理学报 57 6030]
[23] [24] [25] Sun C M, Yuan Y, Zhang X B 2009 Proc. SPIE 7383 381
[26] Xu X H, Liang X G, Ren J X 2006 J. Astron. 27 153 ( in Chinese) [徐向华、梁新刚、任建勋 2006 宇航学报 27 153]
[27] [28] Xi X N, Wang W, Gao Y D 2003 Fundamentals of Near-Earth Spacecraft Orbit (Changsha: National University of Defense Technology Press) p11 ( in Chinese) [郗晓宁、王 威、高玉东 2003 近地航天器轨道基础 (长沙: 国防科学技术大学出版社) 第11页]
[29] [30] Lu W T, Wang S J, Zhang H 2007 Acta Phys. Sin. 56 3655 (in Chinese) [卢伟涛、王顺金、张 华 2007 物理学报 56 3655]
[31] [32] Yu J H, Su Z L 2006 J. Spacec. Telem. Track Comm. Technol. 25 52 ( in Chinese) [余建慧、苏增立 2006 飞行器测控学报25 52]
[33] [34] [35] Shen Y J, Zhang Z M, Tsai B K, DeWitt D P 2001 Int. J. Thermophys. 22 1311
[36] Sun C M, Yuan Y, Zhang X B 2010 Acta Phys. Sin. 59 7523 (in Chinese) [孙成明、袁 艳、张修宝 2010 物理学报 59 7523]
[37]
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