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- W1981879142 abstract "Alignment of carrier-based aircraft inertial navigation system (slave inertial navigation system, SINS for short) onmoving carrier needs velocity and attitude information from carrier inertial navigation system (MINS). If velocity andangular rate of the carrier are compensated, SINS alignment will be the same to static alignment. However, accelerationquantization in MINS will cause velocity error, which will influence the rapidity and accuracy of SINS alignment. Thispaper analyzes the influence of acceleration quantization error on SINS rapid alignment. Numerical simulations areperformed, and the results show that if the quantization frequency of MINS accelerator is 24 KHz, and the correspondentalignment error of SINS is within 0.003° / h , the alignment time can not be less than 300s." @default.
- W1981879142 created "2016-06-24" @default.
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- W1981879142 date "2008-10-10" @default.
- W1981879142 modified "2023-09-23" @default.
- W1981879142 title "Analysis of influence of Master INS acceleration quantization error on rapid transfer alignment" @default.
- W1981879142 doi "https://doi.org/10.1117/12.807489" @default.
- W1981879142 hasPublicationYear "2008" @default.
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