2017
DOI: 10.1016/j.asr.2017.06.007
|View full text |Cite
|
Sign up to set email alerts
|

Low-cost and high performance ultra-tightly coupled GPS/INS integrated navigation method

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
4
1

Citation Types

0
10
0

Year Published

2018
2018
2024
2024

Publication Types

Select...
8
1

Relationship

0
9

Authors

Journals

citations
Cited by 25 publications
(10 citation statements)
references
References 12 publications
0
10
0
Order By: Relevance
“…Inertial measurement units (IMU) measure vehicle accelerations and turn rates that can be combined with the GNSS data to improve the trajectory estimation. This has been demonstrated in several studies [12][13][14][15][16][17]. Depending on the processed GNSS data, different variants can be distinguished.…”
Section: Introductionmentioning
confidence: 86%
“…Inertial measurement units (IMU) measure vehicle accelerations and turn rates that can be combined with the GNSS data to improve the trajectory estimation. This has been demonstrated in several studies [12][13][14][15][16][17]. Depending on the processed GNSS data, different variants can be distinguished.…”
Section: Introductionmentioning
confidence: 86%
“…Equation (31) is the discrete receiver clock residual error model for the ultra‐tight integration navigation filter. Although it has the same form as the general receiver clock error model widely used in the tight integration navigation filter, such as the one presented in [23], their representations are quite different.…”
Section: Integration Navigation Filtermentioning
confidence: 99%
“…In order to ensure that the deviations between incoming GNSS signals and local replicas of them will not cause such unexpected excess, it is necessary to compensate the receiver clock errors in the NCO control generation of ultra‐tight integration. In consequence, the receiver clock model for the ultra‐tight integration navigation filter will be markedly different from the general receiver clock model, such as the one presented in [23], adopted in the tight integration navigation filter.…”
Section: Introductionmentioning
confidence: 99%
“…The positioning estimation is done through different methods, as seen, for instance, in [30]- [34], where is shown the fusion of GPS and INS to bridge the period of GPS outages for vehicular navigation. The authors in [35] use random forest regression to enhance the positioning estimation of an airplane, whereas [40] employs Kalman filtering to a high-performance ultra-tightly coupled GPS/INS. In [36]- [39] is seen the use of adaptive networks to perform the Multisensor Data Fusion.…”
Section: Introductionmentioning
confidence: 99%