DocumentCode
3390610
Title
Application of DGPS simulator in HIL simulation of aerocraft
Author
Wang Liang ; Wu Cheng-fu ; Kang Feng-ju
Author_Institution
North West Polytech. Univ. China, Xi´an
fYear
2008
fDate
10-12 Oct. 2008
Firstpage
562
Lastpage
564
Abstract
In order to resolve the problem that DGPS (differential global positioning system) can not be used in the HIL (hardware-in-loop) simulation of aerocraft, but only simulated by math modeling, a method how to use DGPS in HIL simulation was brought forward on the base of GSS7700GPS simulator and NovAtel DGPS receiver. The DGPS simulation system configuration fig of aerocarft was shown.The trial data of single GPS and DGPS was acquired and plotted in the table. Comparing single GPS trial data with DGPS trial data, it improved that DGPS has more positioning accuracy than single GPS. The method realized that the whole DGPS out-of-doors running process could be simulated realistically in static environment of laboratory. The accuracy and reliability of DGPS simulation of aerocraft were improved greatly by using the method.
Keywords
Global Positioning System; aerospace simulation; differential global positioning system simulator; hardware-in-loop aerocraft simulation; math modeling; Acceleration; Aerodynamics; Computational modeling; Computer networks; Computer simulation; Frequency; Global Positioning System; Receiving antennas; Signal generators; Transceivers;
fLanguage
English
Publisher
ieee
Conference_Titel
System Simulation and Scientific Computing, 2008. ICSC 2008. Asia Simulation Conference - 7th International Conference on
Conference_Location
Beijing
Print_ISBN
978-1-4244-1786-5
Electronic_ISBN
978-1-4244-1787-2
Type
conf
DOI
10.1109/ASC-ICSC.2008.4675423
Filename
4675423
Link To Document