Plug and play innosat ACS simulator
| Format: | Restricted Document |
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| _version_ | 1860797357649559552 |
|---|---|
| building | INTELEK Repository |
| collection | Online Access |
| collectionurl | https://intelek.unisza.edu.my/intelek/pages/search.php?search=!collection407072 |
| date | 2015-10-25 10:59:09 |
| format | Restricted Document |
| id | 12396 |
| institution | UniSZA |
| internalnotes | Wang, Q., Zhang, T. & Song, J. 2009. Study on the Control System of a Hardware-in-Loop Micro-Satellite Simulator. Proceedings of the 2009 IEEE International Conference on Robotics and Biomimetics. December 19-23. 2427-2432. Hall, C., Peck, M. & Schwartz, J. 2003. Historical Review of Spacecraft Simulators. AIAA Journal of Guidance, Control and Dynamics. 26(4): 513-522. Kinnett, R. L. 2010. System Integration and Control of a Low Cost Spacecraft Attitude Dynamics Simulator. M.Sc. Thesis of Aerospace Engineering, Faculty of California Polytechnic State University, San Luis Obispo. Romano, M., Friedman, D. A. & Shay, T. J. 2007. Laboratory Experimentation of Autonomous Spacecraft Approach and Docking to a Collaborative Target. Journal of Spacecraft and Rockets. 44(1): 1-10. Boge, T. & Ma, O. 2011. Using Advanced Industrial Robotics for Spacecraft Rendezvous and Docking Simulation. IEEE International Conference Robotics and Automation (ICRA). 1-4. Boge, T., Wimmer, T., Ma, O. & Zebenay, M. 2011. EPOS−A Robotics-Based Hardware-in-the-Loop Simulator for Simulating Satellite RvD Operations. Finnset, R., Rao, S.K. & Antonsen, J. 2006. Real Time Hardware-in-loop Simulation of ESMO Satellite Attitude Control System. Journal of Modeling, Identification and Control. 27(2): 125-140. Kim, B.M., Velenis, E. , Kriengsiri, P. & Tsiotras, P. 2003. Designing a Low-cost Spacecraft Simulator. IEEE Control Systems Magazine. 23(4): 26-37. Vilathgamuwa, D. M., Yue, X. & Tseng, K. J. 2004. Development and Control of a 3-Axis Motion Simulator for Satellite ADCS Hardware-in-the-Loop Simulation. The 30th Annual Conference at the IEEE Industrial Electronics Society. 524-529. Steurer, M., Bogdan, F., Ren, W., Sloderbeck, M. & Woodruff, S. 2007. Controller and Power Hardware-In-Loop Methods for Accelerating Renewable Energy Integration. IEEE Conference on Power Society General Meeting. 1-4. Ledin, J. A. 1999. Hardware-in-the-loop Simulation. Embedded Systems Programming. 42-60. |
| originalfilename | 6698-01-FH02-FSTK-15-03935.jpg |
| person | UniSZA Unisza unisza |
| recordtype | oai_dc |
| resourceurl | https://intelek.unisza.edu.my/intelek/pages/view.php?ref=12396 |
| spelling | 12396 https://intelek.unisza.edu.my/intelek/pages/view.php?ref=12396 https://intelek.unisza.edu.my/intelek/pages/search.php?search=!collection407072 Restricted Document Article Journal UniSZA Unisza unisza image/jpeg inches 96 96 46 46 1423 756 2015-10-25 10:59:09 1423x756 6698-01-FH02-FSTK-15-03935.jpg UniSZA Private Access Plug and play innosat ACS simulator Jurnal Teknologi This research proposes a novel approach of satellite simulator design where the simulator will be in the form of both software and hardware. A software simulator will represent the satellite dynamics model, incorporating all the operating conditions of the satellite in orbit. The control algorithm for Attitude Control System (ACS) will be implemented on Rabbit Micro Controller (RCM4100) and the dynamics model of Innovative Satellite (InnoSAT) plant in PC have been tested using real-time hardware-in-loop-simulation (HILS) technique. The results that have been obtained show that the InnoSAT ACS simulator can produce as good result as MATLAB simulation for the InnoSAT plants. The MSE values that have been calculated also show that there are a close match between HILS and MATLAB simulation where the MSEs different value are small. From both results, it is enough to verify that the developed protocol working satisfyingly and seems to be possible to be implemented on the actual flight. 76 8 Penerbit UTM Press Penerbit UTM Press 23-26 Wang, Q., Zhang, T. & Song, J. 2009. Study on the Control System of a Hardware-in-Loop Micro-Satellite Simulator. Proceedings of the 2009 IEEE International Conference on Robotics and Biomimetics. December 19-23. 2427-2432. Hall, C., Peck, M. & Schwartz, J. 2003. Historical Review of Spacecraft Simulators. AIAA Journal of Guidance, Control and Dynamics. 26(4): 513-522. Kinnett, R. L. 2010. System Integration and Control of a Low Cost Spacecraft Attitude Dynamics Simulator. M.Sc. Thesis of Aerospace Engineering, Faculty of California Polytechnic State University, San Luis Obispo. Romano, M., Friedman, D. A. & Shay, T. J. 2007. Laboratory Experimentation of Autonomous Spacecraft Approach and Docking to a Collaborative Target. Journal of Spacecraft and Rockets. 44(1): 1-10. Boge, T. & Ma, O. 2011. Using Advanced Industrial Robotics for Spacecraft Rendezvous and Docking Simulation. IEEE International Conference Robotics and Automation (ICRA). 1-4. Boge, T., Wimmer, T., Ma, O. & Zebenay, M. 2011. EPOS−A Robotics-Based Hardware-in-the-Loop Simulator for Simulating Satellite RvD Operations. Finnset, R., Rao, S.K. & Antonsen, J. 2006. Real Time Hardware-in-loop Simulation of ESMO Satellite Attitude Control System. Journal of Modeling, Identification and Control. 27(2): 125-140. Kim, B.M., Velenis, E. , Kriengsiri, P. & Tsiotras, P. 2003. Designing a Low-cost Spacecraft Simulator. IEEE Control Systems Magazine. 23(4): 26-37. Vilathgamuwa, D. M., Yue, X. & Tseng, K. J. 2004. Development and Control of a 3-Axis Motion Simulator for Satellite ADCS Hardware-in-the-Loop Simulation. The 30th Annual Conference at the IEEE Industrial Electronics Society. 524-529. Steurer, M., Bogdan, F., Ren, W., Sloderbeck, M. & Woodruff, S. 2007. Controller and Power Hardware-In-Loop Methods for Accelerating Renewable Energy Integration. IEEE Conference on Power Society General Meeting. 1-4. Ledin, J. A. 1999. Hardware-in-the-loop Simulation. Embedded Systems Programming. 42-60. |
| spellingShingle | Plug and play innosat ACS simulator |
| summary | This research proposes a novel approach of satellite simulator design where the simulator will be in the form of both software and hardware. A software simulator will represent the satellite dynamics model, incorporating all the operating conditions of the satellite in orbit. The control algorithm for Attitude Control System (ACS) will be implemented on Rabbit Micro Controller (RCM4100) and the dynamics model of Innovative Satellite (InnoSAT) plant in PC have been tested using real-time hardware-in-loop-simulation (HILS) technique. The results that have been obtained show that the InnoSAT ACS simulator can produce as good result as MATLAB simulation for the InnoSAT plants. The MSE values that have been calculated also show that there are a close match between HILS and MATLAB simulation where the MSEs different value are small. From both results, it is enough to verify that the developed protocol working satisfyingly and seems to be possible to be implemented on the actual flight. |
| title | Plug and play innosat ACS simulator |
| title_full | Plug and play innosat ACS simulator |
| title_fullStr | Plug and play innosat ACS simulator |
| title_full_unstemmed | Plug and play innosat ACS simulator |
| title_short | Plug and play innosat ACS simulator |
| title_sort | plug and play innosat acs simulator |