Optical system design of visible camera for space debris

Hu Wang, Jianjun Luo

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

In order to detect the space debris, a visible camera for space debris was proposed. The visible camera was mainly consisted of primary mirror, secondary mirror. In order to balance aberration, six correcting lens were used in the optical system. To reduce the visible camera system size, two mirrors were joined, which could fold the system and shorten the overall length. The focal length was 12000 mm, field of view was 1. 0 and the f-number was 10.0. The imaging quafity of the optical system in visible camera approached to diffraction limit.

Original languageEnglish
Title of host publicationInternational Symposium on Photoelectronic Detection and Imaging 2013
Subtitle of host publicationImaging Spectrometer Technologies and Applications
PublisherSPIE
ISBN (Print)9780819497796
DOIs
StatePublished - 2013
Event5th International Symposium on Photoelectronic Detection and Imaging, ISPDI 2013 - Beijing, China
Duration: 25 Jun 201327 Jun 2013

Publication series

NameProceedings of SPIE - The International Society for Optical Engineering
Volume8910
ISSN (Print)0277-786X
ISSN (Electronic)1996-756X

Conference

Conference5th International Symposium on Photoelectronic Detection and Imaging, ISPDI 2013
Country/TerritoryChina
CityBeijing
Period25/06/1327/06/13

Keywords

  • rendezvous and docking
  • Space debris
  • visible camera

Fingerprint

Dive into the research topics of 'Optical system design of visible camera for space debris'. Together they form a unique fingerprint.

Cite this