Abstract
This paper mainly studies the fault tolerance technology of redundant flight control computer based on ARINC 659 bus. A kind of redundant flight control computer architecture based on ARINC 659 bus and its working mode are introduced. In the aspect of fault detection, The control unit and the interface unit detect each other. The heartbeat detection and the state detection are combined. The channel fault logic signal and its usage are introduced. In the aspect of fault handling, a simple and reliable recovery method is presented. Finally, a semi-physical simulation platform is built to verify the effectiveness and correctness of the fault tolerant strategy which can improve the reliability of the flight control computer.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Zhang, X., Wei, T.: Development of ARINC659 fault-tolerant data bus test and verification system. J. Xidian University (Natural Sci. Edn.) 38(6), 140–145 (2011)
Li, A., Zhao, G., Li, W., et al.: Design and implementation of aircraft electrical control system based on 659 bus. Comput. Measurement control 23(4), 1218–1221 (2015)
Tian, Z., Liu, N., Guo, L., et al.: ARINC659 baseplate data bus and key technologies. Comput. Appl. 33(z2), 49–53 (2013)
Tian, Z., Guo, L., Liu, N., et al.: Research on key technologies for verification of protocol compliance of ARINC659 chip. Avionics Technol. 44(1), 37–42 (2013)
Zhang, R., Wu, C., Duan, X., et al.: Application of ARINC659 bus in flight control redundancy management technology. Aviat. Comput. Technol. 43(2), 128–130 (2013)
Zhang, X., Liu, W.: Research and design improvement of electrical characteristics of ARINC659 backplane bus. Comput. Measurement Control 22(10), 3330–3332 (2014)
Ai, J., Wang, P., Gaoming.: Research on the reconstruction technology of flight control system. Firepower Command Control 31(1), 1–3 (2006)
Zhao, H.: Building a smooth path of intelligent spacecraft with integrated electronic technology. Spacecraft Eng. 24(6) (2015)
Pan, J., Zhang, S., Zhang, X.: Research on fault diagnosis and reconstruction technology of flight control system. Comput. Measurement Control 23(4), 1073–1101 (2015)
Pan, J., Zhang, S., Wang, D.: Research on fault-tolerant technology of high-altitude and long-endurance UAV flight control aircraft. J. Northwestern Polytech. University 36(4), 761–767 (2008)
Sun, J., Yang, X.: Design and implementation of MPFTS fault recovery in a multi-machine fault-tolerant system. Comput. Appl. Soft. 10, 4–6 (2001)
Wang, F., Liao, K.: Application research status and development trend of fault-tolerant flight control technology. Flight Mech. 35(1), 1–6 (2017)
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2022 The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.
About this paper
Cite this paper
Shao, H., Cao, D. (2022). Research on Fault Tolerance Technology of Redundant Flight Control Computer Based on ARINC 659 Bus. In: Yan, L., Duan, H., Yu, X. (eds) Advances in Guidance, Navigation and Control . Lecture Notes in Electrical Engineering, vol 644. Springer, Singapore. https://doi.org/10.1007/978-981-15-8155-7_431
Download citation
DOI: https://doi.org/10.1007/978-981-15-8155-7_431
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-15-8154-0
Online ISBN: 978-981-15-8155-7
eBook Packages: Intelligent Technologies and RoboticsIntelligent Technologies and Robotics (R0)