DocumentCode
3085030
Title
Implementation of GPS/INS navigation system using low-cost MEMS sensors
Author
Sun, Chun-Jung ; Hung, Chang-Wen ; Huang, Wei-Cheng ; Lin, Chin E.
Author_Institution
Dept. of Aeronaut. & Astronaut., Nat. Cheng Kung Univ., Tainan, Taiwan
fYear
2010
fDate
15-17 June 2010
Firstpage
1588
Lastpage
1592
Abstract
MEMS technology has drastically improving sensor size, weight, cost and power consumption for high accuracy, high reliability and high stability as a navigation option to low cost systems. The MEMS fabricated INS can be complementary with GPS to enhance the augmentation performance to an acceptable reliability. This paper focuses on implementation of a GPS/INS integrated system including calibration and verification on sensor components and overall operation.
Keywords
Global Positioning System; inertial navigation; microsensors; GPS-INS navigation system; MEMS technology; global positioning system; inertial navigation system; low-cost MEMS sensor; Aircraft navigation; Costs; Degradation; Energy consumption; Global Positioning System; Micromechanical devices; Power system reliability; Sensor systems; Stability; Unmanned aerial vehicles; GPS/INS; MEMS; Microprocessor; Navigation Perfroamnce;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Electronics and Applications (ICIEA), 2010 the 5th IEEE Conference on
Conference_Location
Taichung
Print_ISBN
978-1-4244-5045-9
Electronic_ISBN
978-1-4244-5046-6
Type
conf
DOI
10.1109/ICIEA.2010.5514724
Filename
5514724
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