Paper
8 September 2011 Design of infrared imaging system for inner-formation flying system
DaPeng Han, Longlong Xiao, Zhaokui Wang, Kun Liu
Author Affiliations +
Abstract
This paper describes an infrared Imaging system for the Inner-formation Flying System (IFS), a new kind of spacecraft system to measure Earth's gravity field. Challenges arise when measuring the relative position between the moving inner-satellite and its cavity. The observing process should be real-time and highly precise, with the premise that non-gravitational disturbing force be restrained. An infrared imaging system was proposed for the observation. Challenges were handled via a thermal-electronic-mechanical integration design. With a specially designed electronic component, a dynamic thermal loop and a novel calibration mechanism, an infrared imaging system was established to perform long-time continuous precise measurement. Infrared images with a Signal Noise Ratio better than 2:1 was acquired, being sufficient to acquire accurate position of the inner-satellite. Performance of the imaging system was validated by experiment.
© (2011) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
DaPeng Han, Longlong Xiao, Zhaokui Wang, and Kun Liu "Design of infrared imaging system for inner-formation flying system", Proc. SPIE 8193, International Symposium on Photoelectronic Detection and Imaging 2011: Advances in Infrared Imaging and Applications, 819313 (8 September 2011); https://doi.org/10.1117/12.899558
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CITATIONS
Cited by 6 scholarly publications.
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KEYWORDS
Imaging systems

Infrared imaging

Calibration

Staring arrays

Infrared radiation

Iterated function systems

Signal to noise ratio

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