TROPOSPHERE PARAMETERS CALCULATION AND RESIDUAL ERROR MODELING FOR GNSS LANDING SYSTEM
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Date
2017-05-12
Journal Title
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Publisher
Proceedings of the 20th Conference for Junior Researchers ‘Science – Future of Lithuania’ TRANSPORT ENGINEERING AND MANAGEMENT, 12 May 2017, Vilnius, Lithuania. - P. 63-68
Abstract
The paper shows the results of simulation of troposphere residual errors in the satellite based aircraft landing system. For such simulation the troposphere MOPS model has been used. The presented simulated troposphere parameters
include: dry and wet components of the refraction index and troposphere scale height. Beside of that the simulated residual value of troposphere error for navigation satellites in view of satellite landing system has been presented
Description
Keywords
global navigation satellite systems (GNSS), landing system, GBAS, troposphere, tropospheric delay, modelling