Trade study and application of symbiotic software and hardware fault-tolerance on a microcontroller-based avionics system
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2011. === Cataloged from PDF version of thesis. === Includes bibliographical references (p. 195-201). === Spacecraft avionics initially commanded the development of the microprocessor industry, enabling micr...
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ndltd-MIT-oai-dspace.mit.edu-1721.1-671942019-05-02T15:37:35Z Trade study and application of symbiotic software and hardware fault-tolerance on a microcontroller-based avionics system Trade study and application of software implemented fault-tolerance for microcontroller-based avionics McCormack, Matthew Michael Alvar Saenz-Otero and David W. Miller. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Aeronautics and Astronautics. Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2011. Cataloged from PDF version of thesis. Includes bibliographical references (p. 195-201). Spacecraft avionics initially commanded the development of the microprocessor industry, enabling microprocessors to be designed specifically for the reliability demands posed by the radiation environment of space. However, microprocessor have shifted their focus from ensuring reliable operations to maximizing performance, forcing the price of spacecraft avionics to balloon. Costing over three orders of magnitude more than current state of the art general purpose processors, while performing operations an order of magnitude slower. These differences stem from the reliability requirements of operating in space, typically achieved through hardware-based modifications. While these solutions generate the necessary reliability, they limit the engineering options for the system and force the use of outdated technology. A solution researched but never widely implemented, is the use of error detection and correction software algorithms. An ideal design lies in the combination of hardware and software methods for providing reliability. A new avionics architecture was designed to implement a system using hardware and software to achieve reliability with COTS products. The architecture was applied to the CASTOR satellite as its primary avionics system, for verification testing of the architecture's functionality. This architecture further aims to expand spacecraft usage of microcontrollers as the primary spacecraft avionics computers. by Matthew Michael McCormack. S.M. 2011-11-18T20:58:56Z 2011-11-18T20:58:56Z 2011 2011 Thesis http://hdl.handle.net/1721.1/67194 758673081 eng M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 201 p. application/pdf Massachusetts Institute of Technology |
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Aeronautics and Astronautics. |
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Aeronautics and Astronautics. McCormack, Matthew Michael Trade study and application of symbiotic software and hardware fault-tolerance on a microcontroller-based avionics system |
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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2011. === Cataloged from PDF version of thesis. === Includes bibliographical references (p. 195-201). === Spacecraft avionics initially commanded the development of the microprocessor industry, enabling microprocessors to be designed specifically for the reliability demands posed by the radiation environment of space. However, microprocessor have shifted their focus from ensuring reliable operations to maximizing performance, forcing the price of spacecraft avionics to balloon. Costing over three orders of magnitude more than current state of the art general purpose processors, while performing operations an order of magnitude slower. These differences stem from the reliability requirements of operating in space, typically achieved through hardware-based modifications. While these solutions generate the necessary reliability, they limit the engineering options for the system and force the use of outdated technology. A solution researched but never widely implemented, is the use of error detection and correction software algorithms. An ideal design lies in the combination of hardware and software methods for providing reliability. A new avionics architecture was designed to implement a system using hardware and software to achieve reliability with COTS products. The architecture was applied to the CASTOR satellite as its primary avionics system, for verification testing of the architecture's functionality. This architecture further aims to expand spacecraft usage of microcontrollers as the primary spacecraft avionics computers. === by Matthew Michael McCormack. === S.M. |
author2 |
Alvar Saenz-Otero and David W. Miller. |
author_facet |
Alvar Saenz-Otero and David W. Miller. McCormack, Matthew Michael |
author |
McCormack, Matthew Michael |
author_sort |
McCormack, Matthew Michael |
title |
Trade study and application of symbiotic software and hardware fault-tolerance on a microcontroller-based avionics system |
title_short |
Trade study and application of symbiotic software and hardware fault-tolerance on a microcontroller-based avionics system |
title_full |
Trade study and application of symbiotic software and hardware fault-tolerance on a microcontroller-based avionics system |
title_fullStr |
Trade study and application of symbiotic software and hardware fault-tolerance on a microcontroller-based avionics system |
title_full_unstemmed |
Trade study and application of symbiotic software and hardware fault-tolerance on a microcontroller-based avionics system |
title_sort |
trade study and application of symbiotic software and hardware fault-tolerance on a microcontroller-based avionics system |
publisher |
Massachusetts Institute of Technology |
publishDate |
2011 |
url |
http://hdl.handle.net/1721.1/67194 |
work_keys_str_mv |
AT mccormackmatthewmichael tradestudyandapplicationofsymbioticsoftwareandhardwarefaulttoleranceonamicrocontrollerbasedavionicssystem AT mccormackmatthewmichael tradestudyandapplicationofsoftwareimplementedfaulttoleranceformicrocontrollerbasedavionics |
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1719025039108472832 |