2012
DOI: 10.5370/jeet.2012.7.4.615
|View full text |Cite
|
Sign up to set email alerts
|

Attitude Determination GPS/INS Integration System Design Using Triple Difference Technique

Abstract: -GPS attitude outputs or carrier phase observables can be effectively utilized to compensate the attitude error of the strapdown inertial navigation system. However, when the integer ambiguity is not correctly resolved and/or a cycle slip occurs, an erroneous GPS output can be obtained. If the erroneous GPS output is applied to the attitude determination GPS/INS (ADGPS/INS) integrated navigation system, the performance of the system can be degraded. This paper proposes an ADGPS/INS integration system using the… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1

Citation Types

0
2
0

Year Published

2013
2013
2022
2022

Publication Types

Select...
3
2

Relationship

0
5

Authors

Journals

citations
Cited by 10 publications
(2 citation statements)
references
References 13 publications
0
2
0
Order By: Relevance
“…A solution of GNSS-based AD problem for an aircraft and UAV was provided in a number of research articles [44], [70]- [74]. It is featured by integration with INS unit for more reliable and undisturbed angular estimation.…”
Section: Application Environmentsmentioning
confidence: 99%
“…A solution of GNSS-based AD problem for an aircraft and UAV was provided in a number of research articles [44], [70]- [74]. It is featured by integration with INS unit for more reliable and undisturbed angular estimation.…”
Section: Application Environmentsmentioning
confidence: 99%
“…The receiver that receives the GPS data from the satellite measures its own location information using the signal time and a triangulation method. 10,11 The location services based on GPS, however, have a high error value of 10 m because of a gap between the transmitters and satellite locations. To counter this error value, DGPS and RTK can be used for the transmitter.…”
Section: Gps (Global Positioning System)mentioning
confidence: 99%