TY - GEN
T1 - The assessment of aircraft positioning accuracy using gps data in rtk-otf technique
AU - Ćwiklak, Janusz
AU - Kozuba, Jarosław
AU - Krasuski, Kamil
AU - Jafernik, Henryk
N1 - Publisher Copyright:
© SGEM 2018.
PY - 2018
Y1 - 2018
N2 - The article presents the results of the research studies assessing the accuracy of determining the position of an aircraft using the differential RTK-OTF technique in the post-processing mode. The data for the research test come from an in-flight test in which a Cessna 172 aircraft was used, and which was conducted around the EPDE military airport in Dęblin, Poland. The position of the Cessna 172 aircraft was retrieved in the ASOS v.2.0 program for 3 independent RTK measurements in the OTF positioning mode. For the purposes of the numerical calculations, GPS observations from the REF1 reference station were used, and from two virtual stations, VirA and VirB, as well as from a rover GNSS receiver mounted onboard the Cessna 172 aircraft. The research test also included the presentation and comparison of the results of the aircraft position error in 3D space – the MRSE parameter. The average MRSE error value for the REF1-Cessna base solution is over 0.03 m. The average MRSE error value for the VirA-Cessna base solution is, in turn, below 0.03 m. Moreover, the average MRSE error value for the VirA-Cessna base solution is also below 0.03 m. The article also presents the difference in MRSE parameter values from individual RTK solutions in the OTF mode.
AB - The article presents the results of the research studies assessing the accuracy of determining the position of an aircraft using the differential RTK-OTF technique in the post-processing mode. The data for the research test come from an in-flight test in which a Cessna 172 aircraft was used, and which was conducted around the EPDE military airport in Dęblin, Poland. The position of the Cessna 172 aircraft was retrieved in the ASOS v.2.0 program for 3 independent RTK measurements in the OTF positioning mode. For the purposes of the numerical calculations, GPS observations from the REF1 reference station were used, and from two virtual stations, VirA and VirB, as well as from a rover GNSS receiver mounted onboard the Cessna 172 aircraft. The research test also included the presentation and comparison of the results of the aircraft position error in 3D space – the MRSE parameter. The average MRSE error value for the REF1-Cessna base solution is over 0.03 m. The average MRSE error value for the VirA-Cessna base solution is, in turn, below 0.03 m. Moreover, the average MRSE error value for the VirA-Cessna base solution is also below 0.03 m. The article also presents the difference in MRSE parameter values from individual RTK solutions in the OTF mode.
KW - Aviation test
KW - GPS
KW - Kalman filter
KW - MRSE
KW - RTK-OTF
UR - https://www.scopus.com/pages/publications/85058904137
U2 - 10.5593/sgem2018/2.2/S08.058
DO - 10.5593/sgem2018/2.2/S08.058
M3 - Conference contribution
AN - SCOPUS:85058904137
SN - 9786197408355
T3 - International Multidisciplinary Scientific GeoConference Surveying Geology and Mining Ecology Management, SGEM
SP - 459
EP - 466
BT - Micro and Nano Technologies, Space Technologies and Planetary Science
PB - International Multidisciplinary Scientific Geoconference
T2 - 18th International Multidisciplinary Scientific Geoconference, SGEM 2018
Y2 - 2 July 2018 through 8 July 2018
ER -