Abstract
The guidance system is very important to the security of automatic carrier landing for carrier-based aircraft, while its guidance computer is the control center of this system. For enhancing the security and reliability of the system, avoiding general hitch, and serious consequence taken from it, dissimilar redundancy technology could be applied on the system design. From the practical requirements for security of carrier landing, the structure of the guidance computer has been studied, with dissimilar redundancy technique, and a kind of simplified reliability model has been applied on reliability analysis. This study shows that the designed structure can satisfy the security and reliability design requirements of the carrier landing system.
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Zhong, W., Wu, W., An, G., Ren, J., Yu, S. (2014). Dissimilar Redundancy Structure Design for Carrier Landing Guidance Computer and Reliability Analysis. In: Wang, J. (eds) Proceedings of the First Symposium on Aviation Maintenance and Management-Volume II. Lecture Notes in Electrical Engineering, vol 297. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-54233-6_42
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DOI: https://doi.org/10.1007/978-3-642-54233-6_42
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Publisher Name: Springer, Berlin, Heidelberg
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Online ISBN: 978-3-642-54233-6
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