DocumentCode
3545096
Title
Position accuracy evaluation of GPS receiver under small UAV flight environment
Author
Du, Xiaojing ; Du, Dacheng ; Wang, Kang
Author_Institution
Beijing Inst. of Technol., Beijing, China
fYear
2009
fDate
16-19 Aug. 2009
Firstpage
42429
Lastpage
12086
Abstract
GPS receiver is widely integrated into the autopilot for Small Unmanned Aircraft Vehicle (SUAV). The flight control loop within the autopilot uses the position and velocity information provided by GPS receiver to control the SUVA to flight through the desired path. So for tightly tracking a desired flight path, it is essential that GPS receiver can provide precise-enough position and velocity information. After selecting the RCB-4H GPS receiver, it is of great significant that the receiver undertakes as many necessary tests as possible before a real flight test. By using the facility of GSS6560 GPS simulator, a series of test were designed and conducted on the ground. Here three tests of them which focus on the evaluation of specifications of position accuracy and acquisition time are described in detail, which includes the test design, test data processing and analysis. The results show that the RCB-4H GPS receiver meets some specifications under certain environment.
Keywords
Global Positioning System; aircraft; inertial navigation; position measurement; remotely operated vehicles; velocity measurement; GPS receiver position accuracy evaluation; GSS6560 GPS simulator; RCB-4H GPS receiver; UAV flight environment; acquisition time; flight control loop; position accuracy specification; position information; test data processing; velocity information; Aerospace electronics; Aerospace simulation; Circuit testing; Data analysis; Global Positioning System; Navigation; Position measurement; Software testing; System testing; Unmanned aerial vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Electronic Measurement & Instruments, 2009. ICEMI '09. 9th International Conference on
Conference_Location
Beijing
Print_ISBN
978-1-4244-3863-1
Electronic_ISBN
978-1-4244-3864-8
Type
conf
DOI
10.1109/ICEMI.2009.5274589
Filename
5274589
Link To Document