Browse > Article
http://dx.doi.org/10.5139/JKSAS.2016.44.1.80

Thermal pointing error analysis of the observation satellites with interpolated temperature based on PAT method  

Lim, Jae Hyuk (Korea Aerospace Research Institute, Satellite Mechanical Team)
Kim, Sun-Won (Korea Aerospace Research Institute, Satellite Mechanical Team)
Kim, Jeong-Hoon (Korea Aerospace Research Institute, Satellite Mechanical Team)
Kim, Chang-Ho (Korea Aerospace Research Institute, Satellite Mechanical Team)
Jun, Hyoung-Yoll (Korea Aerospace Research Institute, Satellite Mechanical Team)
Oh, Hyeon Cheol (Korea Advanced Institute of Science and Technology, Department of Mechanical Engineering)
Shin, Chang Min (Korea Advanced Institute of Science and Technology, Department of Mechanical Engineering)
Lee, Byung Chai (Korea Advanced Institute of Science and Technology, Department of Mechanical Engineering)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.44, no.1, 2016 , pp. 80-87 More about this Journal
Abstract
In this work, we conduct a thermal pointing error analysis of the observation satellites considering seasonal and daily temperature variation with interpolated temperature based on prescribed average temperature (PAT) method. Maximum 200 degree temperature excursion is applied to the observation satellites during on-orbit operation, which cause the line of sight (LOS) to deviate from the designated pointing direction due to thermo-elastic deformation. To predict and adjust such deviation, the thermo-elastic deformation analysis with a fine structural finite element model is accomplished with interpolated thermal maps calculated from the results of on-station thermal analysis with a coarse thermal model. After verifying the interpolated temperatures by PAT with two benchmark problems, we evaluate the thermal pointing error.
Keywords
Thermal Pointing Error Analysis; Prescribed Average Temperature; Line of Sight Vector;
Citations & Related Records
Times Cited By KSCI : 3  (Citation Analysis)
연도 인용수 순위
1 Jae Hyuk Lim, Hee-Kwang Eun, Dae-Kwan Kim, Hong-Bae Kim and Sung-Hoon Kim, "Satellite finite element model updating for the prediction of the effect of micro-vibration", Journal of the Korean Society for Aeronautical and Space Sciences, Vol. 42, No. 8, 2014, pp.173-180.   DOI
2 Do-Soon Hwang, "Pointing Error Analysis of Satellite under On-Orbit Thermal Environments", Journal of the Korean Society for Aeronautical and Space Sciences, Vol. 27, No. 1, 1999, pp.145-151.
3 Jin-Hee Kim, Do-Soon Hwang, Juhun Rhee, Sung-Hoon Kim, Ho-Hyung Lee, "Thermal Pointing Error Analysis on LEO Spacecraft", 2001 MSC/NASTRAN User's conference, 2001, pp.1-8.
4 Sun-Won Kim, Jin-Hee Kim, Jang-Jun Lee, Do-Soon Hwang, "Thermal Pointing Error Analysis of Satellite", Journal of Satellite, Information and Communication, Vol. 2, No.1, 2007, pp. 21-26.
5 Jun, Hyoung Yoll, Jung-Hoon Kim, "A study on thermal model reduction and dynamic response", Journal of Computational Fluids engineering, Vol. 19, No. 4, 2014, pp. 37-44.   DOI
6 S. Appel, "SINAS : Generic tool for mapping lumped parameter temperatures to a finite element model for thermo-elastic analyses", 2006, 20th European Workshop on Thermal and ECLS software
7 S. Appel, W. Teichert, "Interpolation of lumped parameter temperatures for thermo-elastic FEM analysis with SINAS", 1996, Proc. Conference on Spacecraft Structures, pp.277-281.
8 J.J.Wijker, Spacecraft Structures, Springer, 2008.
9 European Cooperation for Space Standardization, Space Engineering: Structural finite element models, ECSS-E-ST-32-03C, 2008.