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- W2384908267 abstract "This paper describes the attitude determination system via tight integration of multiple GPS antennae and MEMS based INS.The multiple GPS antennae system can provides attitude via using integer ambiguity solved carrier phase measurement.However,it has problem of the low output rate,latency,and easily lose lock problems.Low-cost MEMS based INS has problems of determining heading and error accumulation.The major objective is to design and implement the reliable attitude determination with high accuracy,high output rate,low latency,quick initialization,robust and redundancy via data fusion of multiple GPS antennae system and the MEMS based INS.The system can provide attitude and other navigation information even without GPS measurements for period of time.Performance analysis shows that the attitude,position,velocity,acceleration,and angular rates are estimated at 200 Hz with accuracy(standard deviation) of 0.08~o/s,1.5 m,0.1 m/s,0.12 m/s~2,and(0.1~o/s).This paper presents the methodology of the technique and performs the analysis based on the methodology." @default.
- W2384908267 created "2016-06-24" @default.
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- W2384908267 date "2006-01-01" @default.
- W2384908267 modified "2023-09-26" @default.
- W2384908267 title "Study on multiple GPS antennae and MEMS based on INS integrated attitude determination system" @default.
- W2384908267 hasPublicationYear "2006" @default.
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