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Communication and Optimization for Satellite Attitudes Using Proportional-Integral-Derivative Controller

M Raja1 , Monish Mathur2 , Ugur Guven3 , Om Prakash4

1 Aerospace Engineering Department, UPES, Dehradun, India.
2 Aerospace Engineering Department, UPES, Dehradun, India.
3 Aerospace Engineering Department, UPES, Dehradun, India.
4 Aerospace Engineering Department, UPES, Dehradun, India.

Section:Research Paper, Product Type: Journal
Vol.7 , Issue.6 , pp.1-6, Dec-2019

Online published on Dec 31, 2019


Copyright © M Raja, Monish Mathur, Ugur Guven, Om Prakash . This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
 

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IEEE Style Citation: M Raja, Monish Mathur, Ugur Guven, Om Prakash, “Communication and Optimization for Satellite Attitudes Using Proportional-Integral-Derivative Controller,” International Journal of Scientific Research in Network Security and Communication, Vol.7, Issue.6, pp.1-6, 2019.

MLA Style Citation: M Raja, Monish Mathur, Ugur Guven, Om Prakash "Communication and Optimization for Satellite Attitudes Using Proportional-Integral-Derivative Controller." International Journal of Scientific Research in Network Security and Communication 7.6 (2019): 1-6.

APA Style Citation: M Raja, Monish Mathur, Ugur Guven, Om Prakash, (2019). Communication and Optimization for Satellite Attitudes Using Proportional-Integral-Derivative Controller. International Journal of Scientific Research in Network Security and Communication, 7(6), 1-6.

BibTex Style Citation:
@article{Raja_2019,
author = {M Raja, Monish Mathur, Ugur Guven, Om Prakash},
title = {Communication and Optimization for Satellite Attitudes Using Proportional-Integral-Derivative Controller},
journal = {International Journal of Scientific Research in Network Security and Communication},
issue_date = {12 2019},
volume = {7},
Issue = {6},
month = {12},
year = {2019},
issn = {2347-2693},
pages = {1-6},
url = {https://www.isroset.org/journal/IJSRNSC/full_paper_view.php?paper_id=377},
publisher = {IJCSE, Indore, INDIA},
}

RIS Style Citation:
TY - JOUR
UR - https://www.isroset.org/journal/IJSRNSC/full_paper_view.php?paper_id=377
TI - Communication and Optimization for Satellite Attitudes Using Proportional-Integral-Derivative Controller
T2 - International Journal of Scientific Research in Network Security and Communication
AU - M Raja, Monish Mathur, Ugur Guven, Om Prakash
PY - 2019
DA - 2019/12/31
PB - IJCSE, Indore, INDIA
SP - 1-6
IS - 6
VL - 7
SN - 2347-2693
ER -

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Abstract :
In the proposed research work to determination of attitude and optimization of control parameters for attitude control and stabilization system. The equations as given to transform Euler angles to Quaternions and vice versa. PID Controller comprises is control loop feedback mechanism. The modelling (MATLAB-SIMULINK) for control parameters are defined and optimized to be actuated via reaction wheels in conjugation with Magneto Torquer. The attitude of the model is determined and then the control equations are adapted so that attitude as stabilized by reaction wheel and the torque rod achieves momentum damping. The stability of the system is demonstrated using Lyapunov function. Numerical simulations has performed on MATLAB to optimize control parameters. Thus, the feasibility and effectiveness of the PID control system as demonstrated.

Key-Words / Index Term :
Quaternion, PID, Wahba’s Loss Function, Lyapunov function

References :
[1] Leo satellites: attitude determination and control components; some linear attitude control techniques by Ceren Kaplan.
[2] Uğur Murat Leloğlu, Gökhan Yüksel, Prof. Sir Martin N. Sweeting, “BILSAT-1: A Case Study For the Survey Satellite Technology Ltd. KnowHow Transfer and Training Programme”, 53rd International Astronautical Congress, 10-19 Oct 2002.
[3] Luis M. Gomes, Gökhan Yüksel, Alex da Silva Ceriel, Andy Bradford, Prof. Sir Martin Sweeting, “BILSAT-1: Advancing Small-Sat Capabilities”, SS C03VI-4, 17th AIAA/USU Conference on Small Satellites.
[4] E. Jerpseth Overby, “Attitude Control for the Norwegian Student Satellite NCube”, M.Sc. Thesis in NTNU, 2004
[5] James R. Wertz, Spacecraft Attitude Determination and Control, Kluwer Academic Publishers, Netherlands, 1997.
[6] Hakkı Özgür Derman, “3-Axis Control of Geostationary Satellite”, M.Sc. Thesis, M.E.T.U. , 1999. [10] Vladimir A. Chobotov, Spacecraft Attitude Dynamics and Control, Krieger Publishing Co., Florida, 1991.
[7] A Multi-mode Attitude Determination and Control System for Small Satellites by W.H. Steyn [11] P.J. Rimroh, Introductory Attitude Dynamics and Control, John Wiley and Sons, USA, 1976.
[8] Kyrkjebo, Erik, “Satellite Attitude Determination, 3-Axis Attitude Determination Using Magnetometers and a Star Tracker”, Sıv. Ing. Thesis, Department of Engineering Cybertechnics, NTNU, 2000.
[9] M. H. Kaplan, Modern Spacecraft Dynamics and Control, John Wiley & Sons, USA, 1976.
[10] Özge Uslu, “Orbit Dynamics, Attitude Dynamics and Control Investigation into Possible Applications to TÜRKSAT”, M.Sc. Thesis in Aeronautical Engineering, M.E.T.U., Ankara, January, 1997.
[11] Chris Hall, “HokieSat Attitude and Orbit Dynamics and Control.”, Aeronautics and Astronautics, University of Illinois, March 31, 2003.
[12] Stian Sondersrod Ose, “Attitude Determination for the Norwegian Student Satellite NCUBE”, M.Sc. Thesis, Department Of Engineering Cybernetics, NTNU, Norway, 2004.
[13] Egeland & Gravdahl , Jan Tommy, Modeling and simulation for control, Lecture Notes, Department of Engineering Cybernetics, NTNU, 2001.
[14] Kristian Svartveit, “Attitude Determination of the NCUBE Satellite”, M.Sc. Thesis in Department Of Engineering Cybernetics, June, 2003.
[15] Mortar Pedersen Topland, “Nonlinear Attitude Control of the Microsatellite ESEO”, M.Sc. Thesis in Department Of Engineering Cybernetics, NTNU, July, 2004.
[16] R. Wisniewski & M. Blanke, “Satellite Attitude Control Using Only Electromagnetic Actuation”, Ph.D. Thesis, Department Of Control Engineering, Aalborg University, Denmark, 1996.
[17] Fullmer Rees, “Attitude Determination and Control”, paper, Mechanical and Aerospace Engineering, Utah University, 1993.
[18] PID Controller Design For The Satellite Attitude Control System by Sami Kadhim Hasan Ar-Ramahi College of Information Engineering, Nahrain University, Baghdad- IRAQ.

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