Abstract/Description
The main objective of this paper is to design a Triple modular redundancy test bench using FRAM (Ferroelectric RAM) based memory module for main driver of OBDH (On Board Data Handling) system of LEO (Lower Earth Orbit) Satellite that enables the fast detection of error in driver data when implied with FPGA (Field Programmable Gate Array) and provides more realistic and tolerant way of fault finding for Single Event Upset (SEU) in highly radiated space environment. The scope of paper embraces development of TMR test bench, software algorithms, functional simulations, timing simulations and conclusion of comparison of FRAM based memory module with EEPROM and Flash Memories.
Location
Room C5
Session Theme
Application of ICT
Session Type
Other
Session Chair
Dr. Arshad Siddiqi
Start Date
24-7-2011 12:20 PM
End Date
24-7-2011 12:40 PM
Recommended Citation
Siddiqui, K. S., & Baig, M. A. (2011). Application of ICT: FRAM based TMR (triple modular redundancy) for fault tolerance implementation. International Conference on Information and Communication Technologies. Retrieved from https://ir.iba.edu.pk/icict/2011/2011/50
Application of ICT: FRAM based TMR (triple modular redundancy) for fault tolerance implementation
Room C5
The main objective of this paper is to design a Triple modular redundancy test bench using FRAM (Ferroelectric RAM) based memory module for main driver of OBDH (On Board Data Handling) system of LEO (Lower Earth Orbit) Satellite that enables the fast detection of error in driver data when implied with FPGA (Field Programmable Gate Array) and provides more realistic and tolerant way of fault finding for Single Event Upset (SEU) in highly radiated space environment. The scope of paper embraces development of TMR test bench, software algorithms, functional simulations, timing simulations and conclusion of comparison of FRAM based memory module with EEPROM and Flash Memories.
