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A Lightweight Method for Detecting and Correcting Errors in Low-Frequency Measurements for In-Orbit Demonstrators.
María-Ángeles Cifredo-Chacón1, José-María Guerrero-Rodríguez1, Ignacio Mateos1
1Electronic and Electromagnetic Design Group, Escuela Superior de Ingeniería, University of Cádiz, Avda. de la Universidad, 10, E-11519 Puerto Real, Cádiz, Spain.
This study introduces a new technique, Cross-Checking and Mirroring (CCM), to protect satellite memory from radiation-induced bit-flips. CCM ensures data integrity in space missions, even with multiple memory errors.
Area of Science:
- Space Science and Engineering
- Aerospace Technology
- Radiation Effects on Electronics
Background:
- In-orbit experiments are crucial for validating new technologies in space.
- Low Earth Orbit (LEO) satellites face radiation hazards causing memory bit-flips.
- Magnetic sensing techniques require robust data integrity in space environments.
Purpose of the Study:
- To evaluate the in-flight performance of magnetic sensing techniques.
- To analyze memory data redundancy and recovery options for space missions.
- To introduce and validate a new technique for ensuring data integrity against radiation effects.
Main Methods:
- Utilized in-orbit demonstrators (MELISA) in LEO.
- Analyzed memory data redundancy using auxiliary flash memory and duplicated data structures.
- Proposed and implemented the Cross-Checking and Mirroring (CCM) technique.
- Evaluated four alternative algorithms based on merit indicators.
Main Results:
- The proposed CCM technique and alternative algorithms demonstrated similar, effective performance.
- The methods are robust against multiple bit-flips in flash memory.
- The computational overhead introduced by CCM is negligible, even for 8-bit microcontrollers.
Conclusions:
- The CCM technique provides a lightweight and effective solution for data integrity in radiation-heavy space environments.
- In-orbit validation of magnetic sensing systems is feasible and essential.
- The developed methods enhance the reliability of electronic systems on LEO satellites.
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