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- W2348542187 abstract "An approach for real-time detecting and isolateing GPS fault in pseudo range and pseudo range rate was presented for tightly integrated missile-borne navigation system composed of SINS and GPS. First,the tightly integration algorithm which takes GPS pseudo range and pseudo range rate directly as measurements was deduced based on SINS navigation error model and Kalman filtering theory. On the basis,a GPS fault detection method based on residual chi-square test and a GPS fault isolation method based on Chebyshev theorem ware designed through analyzing statistical characteristics of the filter residual. Simulation results showed that the proposed algorithm can further improve the system in anti-interference ability and thus guarantee navigation accuracy effectively when-fault occurs to information from one or more satellites occur fault." @default.
- W2348542187 created "2016-06-24" @default.
- W2348542187 creator A5012628375 @default.
- W2348542187 date "2014-01-01" @default.
- W2348542187 modified "2023-09-25" @default.
- W2348542187 title "SINS Aided GPS Monitoring Technique Applied in Integrated Missile-borne Navigation System" @default.
- W2348542187 hasPublicationYear "2014" @default.
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