2005
DOI: 10.1007/s10291-005-0135-9
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Design of a low-cost attitude determination GPS/INS integrated navigation system

Abstract: Due to their complementary features of GPS and INS, the GPS/INS integrated navigation system is increasingly being used for a variety of commercial and military applications. An attitude determination GPS (ADGPS) receiver, with multiple antennas, can be more effectively integrated with a low-cost IMU since the receiver gives not only position and velocity data but also attitude data. This paper proposes a low-cost attitude determination GPS/INS integrated navigation system. The proposed navigation system compr… Show more

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Cited by 36 publications
(16 citation statements)
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“…Regarding hardware, future work will include the use of low cost sensors, e.g. antenna array receiver based on GPS L1 or low cost IMU as in Hwang et al (2005). Side-viewing scanning is certainly suitable to capture laminar spatial data like building facades.…”
Section: Discussionmentioning
confidence: 99%
“…Regarding hardware, future work will include the use of low cost sensors, e.g. antenna array receiver based on GPS L1 or low cost IMU as in Hwang et al (2005). Side-viewing scanning is certainly suitable to capture laminar spatial data like building facades.…”
Section: Discussionmentioning
confidence: 99%
“…However, the INS has a drawback in that errors accumulate over time, especially in the case of a low-cost MEMS-INS. If the GPS and MEMS-INS are combined effectively, the reliability and accuracy of attitude determination can be improved [32][33][34].…”
Section: Methodsmentioning
confidence: 99%
“…In order to reduce the effect of large outliers in pseudorange on the float ambiguity solution, a simple quality control (QC) method is adopted here, which is based on the residual chi-square test [ 6 , 10 ]. As the float solution is calculated by LSQ method, the key issue is how to construct the residual vector.…”
Section: Improved Attitude Determination Methods For Single Frequenmentioning
confidence: 99%
“…The drawback of INS is that the errors are accumulated over time especially for the low-cost MEMS-INS. If the GPS and MEMS-INS are combined effectively, the reliability and accuracy of attitude determination can be improved [ 5 , 6 , 7 ].…”
Section: Introductionmentioning
confidence: 99%