ANALYSIS ON ATTITUDE POSITION OF EARTH CENTERED INERTIAL (ECI) BASED ON RAZAKSAT DATA

Authors

  • Mohd Zamri Hasan Faculty of Engineering Technology, Universiti Malaysia Perlis, Perlis, Malaysia
  • Sazali Yaacob School of Mechatronic, Universiti Malaysia Perlis, Perlis, Malaysia
  • Amran Ahmed Institute of Mathematical Engineering, Universiti Malaysia Perlis, Perlis, Malaysia
  • Nor Hazadura Hamzah Institute of Mathematical Engineering, Universiti Malaysia Perlis, Perlis, Malaysia
  • Shamshul Bahar Yaakob School of Electrical System Engineering, Universiti Malaysia Perlis, Perlis, Malaysia
  • Muhd Hafizi Idris School of Electrical System Engineering, Universiti Malaysia Perlis, Perlis, Malaysia
  • Md Azlin Md Said School of Civil Engineering, Engineering Campus, Universiti Sains Malaysia, Pulau Pinang, Malaysia

DOI:

https://doi.org/10.11113/jt.v76.5887

Keywords:

Attitude position, Earth Centered Inertial (ECI), velocity, RazakSAT, Satellite Tools Kit (STK)

Abstract

Attitude determination system (ADS) is a process to control the orientation of satellite to make sure that the orientation of satellite is relative to inertial reference frame such as Earth. Earth Centered Inertial (ECI) is one of reference frame for satellite that determines the attitude in three dimensional spacecraft. Since RazakSAT orbits on earth, ECI coordinate system will be used for satellite relative to earth rotation. This paper is about the analysis on attitude position of ECI and velocity at X, Y and Z axis based on RazakSAT data. Satellite Tools Kit (STK) is used to estimate the attitude and velocity based on Two Line Elements (TLE) of RazakSAT. The result is compared with RazakSAT measurement data to observe the accuracy of estimation by using STK.

References

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Published

2015-10-13

Issue

Vol. 76 No. 12: Man-Machine Systems

Section

Science and Engineering

License

Copyright of articles that appear in Jurnal Teknologi belongs exclusively to Penerbit Universiti Teknologi Malaysia (Penerbit UTM Press). This copyright covers the rights to reproduce the article, including reprints, electronic reproductions, or any other reproductions of similar nature.

How to Cite

ANALYSIS ON ATTITUDE POSITION OF EARTH CENTERED INERTIAL (ECI) BASED ON RAZAKSAT DATA. (2015). Jurnal Teknologi, 76(12). https://doi.org/10.11113/jt.v76.5887