Analysis the Condition of RazakSAT Based on Attitude Sensor of Atttitude Determination System Data

Abstract:

Attitude determination system (ADS) is a process to control the orientation of the satellite to make sure that the orientation is relative to inertial references frame such as Earth. ADS is consists of mathematical algorithm and sensor as a references measurement to determine attitude of satellite. Since RazakSAT in the orbit, the sensor such as sun sensor, magnetometer and gyroscopes are used to control angular rotation and prevent high spin rates that can damage the satellite. This paper presents the analysis on sensor of attitude determination system based on RazakSAT data. Matlab was used to analyze the X,Y and Z axis of the sensor to determine the condition of the satellite.

• Periodical: Applied Mechanics and Materials (Volume 785)
• Pages: 739-743
• DOI: https://doi.org/10.4028/www.scientific.net/AMM.785.739
• Online since: August 2015
• Authors: Mohd Zamri Hasan, Sazali Yaacob, Amran Ahmed, Shamshul Bahar Yaakob, Muhd Hafizi Idris, Md Azlin Md Said
• Keywords: Attitude Determination System, Gyroscopes, Magnetometer, RazakSAT, Sun Sensor

References

[1] J. R. Wertz, Attitude Determination and Control. Boston: Kluwer Academic Publisher, (1978).

[2] Wiley J. Larson, J.R. Wertz, Space Mission Analysis and Design, Third Edition, (1999).

[3] Marcel J. Sidi, Spacecraft Dynamics and Control, A Practical Enigneering Approach, Cambridge University Press, (2000).

[4] S. M. Sharun, Development of an Adaptive Neurol-Sontroller and Satellite Simulator for Nano-Satellite Attitude Control System, PhD Thesis (2012).

[5] Information on http: /projekter. aau. dk/projekter/files/32312420/thesis_10gr1035. pdf.

[6] M. A. M. Said, M. Fadly, O. Sidek, A. Ain, M. F. Alaudin, H. Djojodihardjo, R. Razali, Low Cost Space Experimental Attitude Determination Systems (SEADS) for INNOSAT Project, Proceedings, The 8th CSA-IAA Conference on Advanced Space Technology, 20-23 May 2013, Shanghai, China.

DOI: 10.12928/telkomnika.v9i3.752

[7] M. P. K. A. Ain, Development and Implementation of Embedded Attitude Based termination System Using Extended Kalman Filter Based on ARM7TDMI Platform, MSc Thesis, USM (2013).

[8] B. Andresen, C. GrØn,R. H. Knudsen, C. Nielsen, K. K. Sørensen, D. Taagard, Attitude Control System for AAUSAT-II, Institute of Electronic Systems, Aalborg University. (2005).

[9] Y. Winetraub, S. Bitan, Uvaldd, A. B. Heller, Attitude Determination – Advanced Sun Sensor for Pico- Satellit, Handasaim School, Tel Aviv University, Israel.