Skip to main content
Log in

Determining the heat flux absorbed by satellite surfaces with temperature data

  • Published:
Journal of Mechanical Science and Technology Aims and scope Submit manuscript

Abstract

This study aims to determine the heat flux absorbed by satellite surfaces with the use of temperature data acquired from the satellite. This process is the first step in the development of an attitude determination method, which is currently being conducted by the authors. The principles of heat flux determination and its limitations are explained. A simple heat flux sensor is proposed in this study to address such limitations. With sufficient temperature data, an inverse solution of the energy equation can be used to determine the heat fluxes absorbed by heat flux sensors. The accuracy of the method depends on the resolution of the sensors used to acquire temperature data. The effects of temperature sensor resolution on the accuracy of the results are discussed in this paper.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

References

  1. James R. Wertz and Wiley J. Larson, Space mission analysis and design, Chapter 11, 3rd edition, Microcosm Press and Kluwer Academic Publishers (1999).

    Google Scholar 

  2. [2]Liu Cheng, Zhou Zhaoying and Fu Xu, Attitude determination for MAVs using a Kalman filter, Tsinghua Science and Technology, ISSN 1007-0214 03/25, 13(5) October (2008) 593–597.

    Article  Google Scholar 

  3. Francois Martel, Parimal K. Pal and Mark L. Psi, Three-axis attitude determination via Kalman filtering of magnetometer data, Paper No. 17 for the Flight Mechanics fist Imation Theory Symposium, NASA Goddard Space Flight Center, Greenbelt, Maryland, May 10 & 11 (1988).

    Google Scholar 

  4. Lauren Viscito and Michael C. Cerise, Rate and attitude determination using solar array currents, United States Air Force Academy, Colorado Springs, CO, 80841, American Institute of Aeronautics and Astronautics.

  5. Jacob Daniel DiMiceli, Attitude determination of a student satellite using on-orbit magnetometer and temperature data, California Polytechnic State University, San Luis Obispo, June (2009).

    Book  Google Scholar 

  6. F. Santoni and F. Bolotti, Attitude determination of small spinning spacecraft using three axis magnetometer and solar panels data, Universith degli Studi di Roma “la Sapienza”, Scuola di Ingegneria Aerospaziale, Roma, Italia.

  7. James V. Beck, Inverse heat conduction, Chapter 2, 1st ed., Wiley-Interscience (1985).

    Google Scholar 

  8. J. R. Shenefelt, R. Luck, R. P. Taylor and J. T. Berry, Solution to inverse heat conduction problems employing singular value decomposition and model-reduction, International Journal of Heat and Mass Transfer, 45 (2002) 67–74.

    Article  MATH  Google Scholar 

  9. Michal Cialkowski, A sequential and global method of solving an inverse problem of heat conduction equation, Journal of Theoretical and Applied Mechanics, 48(1) Warsaw (2010) 111–134.

    Google Scholar 

  10. H. J. Reinhardt and Dinh Nho Hào, A sequential conjugate gradient method for the stable numerical solution to inverse heat conduction problems, Inverse Problems in Engineering, 2(4) (1996) 263–272.

    Article  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to S. M. Hossein Karimian.

Additional information

Recommended by Associate Editor Jun Sang Park

S. M. Hossein Karimian has been a professor at the Aerospace Engineering Department of the Amirkabir University of Technology (I.R.IRAN) since 1995. He studied mechanical engineering at the Amirkabir University of Technology (B.Sc.), the Sharif University of Technology (M.Sc.), and the University of Waterloo (Ph.D.). His research interests include computational fluid dynamics and heat transfer, numerical algorithms for incompressible and compressible flows, internal and external flow simulations, aerodynamics of vehicles and buildings, thermal analysis, wind renewable energy, and molecular dynamic simulation. He has published more than 40 papers in refereed journals and more than 80 papers in international and national conference proceedings.

Hojjat Behrooz Khaniki is a Ph.D. student at the Aerospace Engineering Department of the Amirkabir University of Technology (I.R.IRAN). He studied mechanical engineering at the K.N.T. University of Technology (B.Sc.) and Azad University (M.Sc.). His research interests include heat transfer and satellite thermal control. He has published about 10 papers in refereed journals and international and national conference proceedings.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Khaniki, H.B., Hossein Karimian, S.M. Determining the heat flux absorbed by satellite surfaces with temperature data. J Mech Sci Technol 28, 2393–2398 (2014). https://doi.org/10.1007/s12206-014-0531-6

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s12206-014-0531-6

Keywords

Navigation