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CLC number: V447
On-line Access: 2024-08-27
Received: 2023-10-17
Revision Accepted: 2024-05-08
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Infrared Earth sensor with a large field of view for low-Earth-orbiting micro-satellites
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Hao Wang, Zhi-yuan Wang, Ben-dong Wang, Zhong-he Jin, John L. Crassidis. Infrared Earth sensor with a large field of view for low-Earth-orbiting micro-satellites[J]. Frontiers of Information Technology & Electronic Engineering, 2021, 22(2): 262-271.
@article{title="Infrared Earth sensor with a large field of view for low-Earth-orbiting micro-satellites",
author="Hao Wang, Zhi-yuan Wang, Ben-dong Wang, Zhong-he Jin, John L. Crassidis",
journal="Frontiers of Information Technology & Electronic Engineering",
volume="22",
number="2",
pages="262-271",
year="2021",
publisher="Zhejiang University Press & Springer",
doi="10.1631/FITEE.1900358"
}
%0 Journal Article
%T Infrared Earth sensor with a large field of view for low-Earth-orbiting micro-satellites
%A Hao Wang
%A Zhi-yuan Wang
%A Ben-dong Wang
%A Zhong-he Jin
%A John L. Crassidis
%J Frontiers of Information Technology & Electronic Engineering
%V 22
%N 2
%P 262-271
%@ 2095-9184
%D 2021
%I Zhejiang University Press & Springer
%DOI 10.1631/FITEE.1900358
TY - JOUR
T1 - Infrared Earth sensor with a large field of view for low-Earth-orbiting micro-satellites
A1 - Hao Wang
A1 - Zhi-yuan Wang
A1 - Ben-dong Wang
A1 - Zhong-he Jin
A1 - John L. Crassidis
J0 - Frontiers of Information Technology & Electronic Engineering
VL - 22
IS - 2
SP - 262
EP - 271
%@ 2095-9184
Y1 - 2021
PB - Zhejiang University Press & Springer
ER -
DOI - 10.1631/FITEE.1900358
Abstract: infrared Earth sensors are widely used in attitude-determination and control systems of satellites. The main deficiency of static infrared Earth sensors is the requirement of a small field of view (FOV). A typical FOV for a static infrared Earth sensor is about 20° to 30°, which may not be sufficient for low-Earth-orbiting micro-satellites. A novel compact infrared Earth sensor with an FOV of nearly 180° is developed here. The Earth sensor comprises a panoramic annular lens (PAL) and an off-the-shelf camera with an uncooled complementary-metal-oxide-semiconductor (CMOS) infrared sensor. PAL is used to augment FOV so as to obtain a complete infrared image of the Earth from low-Earth-orbit. An algorithm is developed to compensate for the distortion caused by PAL and to calculate the vector of the Earth. The new infrared Earth sensor is compact with low power consumption and high precision. Simulated images and on-orbit infrared images obtained via the micro-satellite ZDPS-2 are used to assess the performance of the new infrared Earth sensor. Experiments show that the accuracy of the Earth sensor is about 0.032°.
[1]Alperovich V, Topaz JM, 1995. Correction of errors due to profile shape in static Earth horizon sensors. Proc 9th Meeting on Optical Engineering in Israel, p.336-344.
[2]Chen TC, Chung KL, 2001. An efficient randomized algorithm for detecting circles. Comput Vis Image Underst, 83(2):172-191.
[3]Crassidis JL, Markley FL, 2016. Three-axis attitude estimation using rate-integrating gyroscopes. J Guid Contr Dynam, 39(7):1513-1526.
[4]Deng LL, Mei ZW, Tu ZJ, et al., 2013. A carbon dioxide radiance model of the Earth planet using the conical Earth sensor data. Proc SPIE Remote Sensing, Article 888 91U.
[5]Falbel G, 2004. A low weight/power/cost infrared Earth sensor. Proc IEEE Aerospace Conf, p.2716-2722.
[6]Gontin R, Ward K, 1987. Horizon sensor accuracy improvement using Earth horizon profile phenomenology. Proc Guidance, Navigation and Control Conf, p.1495-1502.
[7]Gonzalez RC, Woods RE, Eddins SL, 2013. Digital Image Processing Using MATLAB. Prentice-Hall, Inc., Upper Saddle River, USA.
[8]Hoffman JW, 1976. Stability of the infrared Earth horizon at 15 microns. J Spacecr Rock, 13(10):626-628.
[9]Leavers VF, 1993. Which Hough transform? CVGIP Image Underst, 58(2):250-264.
[10]MAI-SES, 2016. Static Earth Sensor Product Specification. Maryland Aerospace Inc., Crofton, USA. https://www.cubesatshop.com/wp-content/uploads/2016/06/MAI-SES-Specifications-20150827.pdf [Accessed on July 20, 2019].
[11]Markley FL, Crassidis JL, 2014. Fundamentals of Spacecraft Attitude Determination and Control. Springer, New York, USA.
[12]Nguyen T, Cahoy K, Marinan A, 2018. Attitude determination for small satellites with infrared Earth horizon sensors. J Spacecr Rock, 55(6):1466-1475.
[13]Niu S, Bai J, Hou XY, et al., 2007. Design of a panoramic annular lens with a long focal length. Appl Opt, 46(32):7850-7857.
[14]Sharifi M, Fathy M, Mahmoudi MT, 2002. A classified and comparative study of edge detection algorithms. Proc Int Conf on Information Technology: Coding and Computing, p.117-120.
[15]Soto-Romero G, Bony F, Simonne JJ, et al., 2001. Micro infrared Earth sensor project: an integrated IR camera for Earth remote sensing. Int Symp on Remote Sensing, p.176-187.
[16]Swartwout M, 2013. The first one hundred CubeSats: a statistical look. J Small Satell, 2(2):213-233.
[17]Torii A, Imiya A, 2007. The randomized-Hough-transform-based method for great-circle detection on sphere. Patt Recogn Lett, 28(10):1186-1192.
[18]Zhang GJ, Wei XG, Fan QY, et al., 2009 Method and Device for Calibration of Digital Celestial Sensor. US Patent 7 822 572.
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