Referenced Items are not available for this document.
The GPS/SINS/BARO integrated system can provide high dynamic and accuracy navigation for UAV flight. In this paper, a GPS/SINS/BARO integrated system for UAV is presented. The system consists of a GPS receiver, an MEMS-based inertial measurement unit (IMU), a Barometer and a navigation processing unit. The GPS receiver provides three-dimensional velocity and position, the IMU provides three-dimensional linear accelerations and angular rates, the barometer provides the altitude of the vehicle indirectly, and the navigation processing unit performs real-time navigation computation with these measurements. The performance of the proposed GPS/SINS/BARO integrated system has been tested with a quad-rotor named `X500-D'. The results show that the integrated system can provide high accuracy navigation for the guidance and control of the UAV.
Published in:
Information Technology and Applications (IFITA), 2010 International Forum on
(Volume:3
)
Date of Conference: 16-18 July 2010
- Page(s):
- 19 - 25
- E-ISBN :
- 978-1-4244-7622-0
- Print ISBN:
- 978-1-4244-7621-3
- INSPEC Accession Number:
- 11648528
- Conference Location :
- Kunming
- Digital Object Identifier :
- 10.1109/IFITA.2010.331
- Product Type:
- Conference Publications
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