2013
DOI: 10.1007/s00006-013-0395-3
|View full text |Cite
|
Sign up to set email alerts
|

Strapdown INS/GPS Integrated Navigation Using Geometric Algebra

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3

Citation Types

0
3
0

Year Published

2016
2016
2021
2021

Publication Types

Select...
4
1
1

Relationship

0
6

Authors

Journals

citations
Cited by 6 publications
(3 citation statements)
references
References 14 publications
0
3
0
Order By: Relevance
“…Such a system utilises specific forces (accelerometer output) and angular rates (gyro output) in three dimensions. Nonetheless, considering the intrinsic bias errors of gyros and accelerometers, INS is usually unable to perform navigation tasks independently in the presence of such gradually increasing errors (Wu and Wang, 2013;Ning et al, 2015;Shabani and Gholami, 2016). Hence, INS should adopt auxiliary sensors in order to provide the required measurements for improving navigation performance.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…Such a system utilises specific forces (accelerometer output) and angular rates (gyro output) in three dimensions. Nonetheless, considering the intrinsic bias errors of gyros and accelerometers, INS is usually unable to perform navigation tasks independently in the presence of such gradually increasing errors (Wu and Wang, 2013;Ning et al, 2015;Shabani and Gholami, 2016). Hence, INS should adopt auxiliary sensors in order to provide the required measurements for improving navigation performance.…”
Section: Introductionmentioning
confidence: 99%
“…In ocean navigation, since satellite signals are repeatedly attenuated, and GPS signals are unavailable, it is necessary to adopt other auxiliary sensors. For underwater navigation, Doppler velocity log (DVL) measures velocity with respect to the seafloor based on the Doppler effect, with high precision (Wu et al., 2019). The emission of acoustic waves by wave-absorbing materials, or large roll and pitch caused by angular manoeuvres, are causes of malfunction of this sensor.…”
Section: Introductionmentioning
confidence: 99%
“…The IMU is composed of gyroscopes and accelerometers to measure the angular rates and the specific forces respectively. The navigation errors of the SINS increase with time due to the inherent bias errors of gyroscopes and accelerometers [3][4][5]. Therefore, in order to improve the navigation performance, it is necessary to introduce auxiliary sensors to limit the error growth of the SINS.…”
Section: Introductionmentioning
confidence: 99%