一种空间视觉测量子系统用半导体激光器驱动电路设计

doi:10.3969/j.issn.1674-1579.2016.02.009

Abstract

Abstract: Abstract：To improve the reliability， accuracy and stray light suppression ability，laser diode is commonly used for illumination of space vision measurement subsystem which is used in rendezvous and docking and onorbit operation mission. A design of laser diode driving circuit is proposed, the delayed start ability, constantcurrent driving and overcurrent protection are realized. Experimental results validate the high stability reliability and high accuracy of proposed designing.

Key words: Keywords：space vision measurement, illuminating light source, laser diode, constantcurrent driving

CLC Number:

WANG Dong-Ning, ZHANG Lin, HUA Bao-Cheng, ZHENG Yan, GONG De-Zhu, ZHAO Chun-Hui. Design of Laser Diode Driving Circuit Used in Space Vision Measurement Subsystem[J]., 2016, 42(2): 49-52.

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URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/10.3969/j.issn.1674-1579.2016.02.009

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2016/V42/I2/49

References

参考文献［1］赵春晖，高文文，刘鲁，等. 神舟八号飞船交会对接CCD光学成像敏感器［J］. 空间控制技术与应用，2011，37（6）：7-14. ZHAO C H, GAO W W, LIU L, et al. A vision guidance sensor for SZ8 spacecraft autonomous rendezvous and docking［J］. Aerospace Control and Application, 2011,37（6）:7-14. ［2］赵春晖，龚德铸，刘鲁，等. 空间杂光对交会对接光学成像敏感器影响分析［J］. 空间控制技术与应用，2012,38（3）：1-4. ZHAO C H, GONG D Z, LIU L, et al. Analysis on influence of space stray light on vision sensor for autonomous rendezvous and docking［J］.Aerospace Control and Application, 2012,38（3）：1-4. ［3］龚德铸，赵春晖，张琳，等.交会对接光学成像敏感器的LD照明系统［J］. 空间控制技术与应用，2014，40（5）：57-62. GONG D Z, ZHAO C H, ZHANG L, et al. LD lighting system for cameratype rendezvous and docking sensor［J］. Aerospace Control and Application, 2014,40（5）:57-62. ［4］张淑琴. 空间交会对接测量技术及工程应用［M］.北京：宇航出版社，2005. ［5］DAVIS C C. Laser Fundmentals激光基础［M］.北京：电子工业出版社，2003：12-28. ［6］王德，李学千.半导体激光器的最新进展及其应用现状［J］. 光学精密工程，2001，9（3）：279-283. WANG D, LI X Q. New progress in semiconductor lasers and their applications［J］. Optics and Precision Engineering, 2001，9（3）：279-283. ［7］黄德修，刘雪峰. 半导体激光器及其应用［M］.北京：国防工业出版社，1999. ［8］何成林.半导体激光器驱动电路设计［J］. 科学技术与工程，2009，9（21）：6532-6535. HE C L. Design of driving circuit of LD［J］. Science Technology and Engineering, 2001，2009，9（21）：6532-6535.

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Design of Laser Diode Driving Circuit Used in Space Vision Measurement Subsystem

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