2014
DOI: 10.3390/s140711395
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The Inertial Attitude Augmentation for Ambiguity Resolution in SF/SE-GNSS Attitude Determination

Abstract: The Unaided Single Frequency/Single Epoch Global Navigation Satellite System (SF/SE GNSS) model is the most challenging scenario for ambiguity resolution in the GNSS attitude determination application. To improve the performance of SF/SE-GNSS ambiguity resolution without excessive cost, the Micro-Electro-Mechanical System Inertial Measurement Unit (MEMS-IMU) is a proper choice for the auxiliary sensor that carries out the inertial attitude augmentation. Firstly, based on the SF/SE-GNSS compass model, the Inert… Show more

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Cited by 9 publications
(6 citation statements)
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“…Since the attitude errors of MEMS-INS are estimated and corrected by the GPS/MEMS-INS integrated filter in real time, which will be introduced in Section 4 , the errors usually are not very large [ 13 , 20 ]. Thus the float solution calculated by MEMS-INS attitude can be regarded as the reference.…”
Section: Improved Attitude Determination Methods For Single Frequenmentioning
confidence: 99%
See 1 more Smart Citation
“…Since the attitude errors of MEMS-INS are estimated and corrected by the GPS/MEMS-INS integrated filter in real time, which will be introduced in Section 4 , the errors usually are not very large [ 13 , 20 ]. Thus the float solution calculated by MEMS-INS attitude can be regarded as the reference.…”
Section: Improved Attitude Determination Methods For Single Frequenmentioning
confidence: 99%
“…LAMBDA is popular for ambiguity resolution, since it is known to maximize the ambiguity success rate [ 9 , 16 ]. It has been used to obtain precise baseline estimations that are then used to extract the platform attitude [ 17 , 18 , 19 , 20 ]. However, the LAMBDA method does not include the prior knowledge of the length of the baseline, which is usually known in GPS attitude determination problems [ 9 , 21 ].…”
Section: Introductionmentioning
confidence: 99%
“…Various constraints can be used to improve the success rate of the ambiguity resolution such as the rate-gyro-constraint from the inertial sensor [11,12] and an a priori baseline vector constraint [1]. For land vehicles, the baseline vector often lies in a small spherical zone, which provides an important constraint for improving the success rate of ambiguity resolution.…”
Section: Improvement In Success Rate Employing Constraintsmentioning
confidence: 99%
“…In contrast to the AFM, the statistical properties of differential measurements are fully exploited in the AOF, thereby achieving dramatic improvements in the success rates. Recent advances on this topic focused on the design of the AOF containing more constraints or prior information such as rate-gyro-constraints from inertial sensors and the prior baseline vector constraints [1,11,12].…”
Section: Introductionmentioning
confidence: 99%
“…The necessary multiple auxiliary receivers and antennas increase system cost, however, limiting the use of this type of scheme in land vehicle applications. Recent studies have integrated inertial and magnetic field sensor measurements into the GPS attitude determination model in order to utilize multiple constraints to decrease the ambiguity search space (Gebre-Egziabher et al 1998;Li et al 2006Li et al , 2012Roth et al 2012;Eling et al 2013;Zhu et al 2013Zhu et al , 2014. For example, Zhu et al (2013) applied rate-gyro-constraints to filter the candidates in the ambiguity search stage, resulting in high ambiguity search success rates after efficiently shrinking the search space.…”
Section: Introductionmentioning
confidence: 99%