Design and Simulation of an Improved Five Redundancy GNC System Architecture

Yue Lin; Ya Nan Gao; Song Tao Fan; Chun Xu

doi:10.4028/www.scientific.net/AMM.543-547.1423

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 543-547Design and Simulation of an Improved Five...

Design and Simulation of an Improved Five Redundancy GNC System Architecture

Abstract:

Aerospace plane, the next generation manned spacecraft has the characteristics of high reliability and high security. Therefore, a five modular redundancy byzantine fault tolerant architecture is propose for the guidance, navigation and control (GNC) system. This architecture can give the system characteristic of double fault resilience, and is also suitable for solving Byzantine general problem. A semi-physical simulation is done, which is based on 1553B data bus and VxWorks operating system. The simulation result has verified the fault tolerant architecture and feasibility of the system implementation.

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Periodical:

Applied Mechanics and Materials (Volumes 543-547)

Pages:

1423-1427

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.543-547.1423

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Online since:

March 2014

Authors:

Yue Lin*, Ya Nan Gao, Song Tao Fan, Chun Xu

Keywords:

Aerospace Plane, Byzantine Fault Resilience, Five Redundant, GNC System

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* - Corresponding Author

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