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 :
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