The integrated navigation system, consisting of barometric altimeter (Baro) and GPS, is presented. The integration is achieved by using a Kalman filtering type data fusion algorithm. The proposed data fusion algorithm utilizes the barometric altimeter and GPS measurements in the estimation procedure in order to increase the altitude estimation accuracy. The performance of the proposed Baro/GPS integrated system is evaluated by the simulations for altitude estimation of an aircraft.
Data Fusion for Integrated Baro/GPS Altimeter
2019-06-01
257555 byte
Conference paper
Electronic Resource
English
An Integrated GPS/INS/BARO and Radar Altimeter System for Aircraft Precision Approach Landing
British Library Conference Proceedings | 1995
|A New Design of Doppler Radar/FOG-SINS/Baro-altimeter Integrated Navigation System for Helicopters
British Library Conference Proceedings | 2011
|European Patent Office | 2024
|BARO algorithm and application in equipment fault diagnosis
Automotive engineering | 2012
|