Long Range Differential Corrections Transmission for Airborne GNSS-based Guidance System

G. Sachs, J. Dittrich, M. Dieroff

Abstract:	A guidance system is considered using computer generated synthetic vision and high precision navigation. A three-dimensional image of the outside world is generated by a computer using a stored data base. The required high navigation precision is achieved by an integrated navigation system using inertial and differential global navigation satellite data. A long range differential correction capability is provided by a ground reference station transmitter operating in a low frequency mode. Flight tests were successfully conducted in a river valley with steep banks and highly curved bends.
Published in:	Proceedings of the 1996 National Technical Meeting of The Institute of Navigation January 22 - 24, 1996 Loews Santa Monica Hotel Santa Monica, CA
Pages:	659 - 667
Cite this article:	Sachs, G., Dittrich, J., Dieroff, M., "Long Range Differential Corrections Transmission for Airborne GNSS-based Guidance System," Proceedings of the 1996 National Technical Meeting of The Institute of Navigation, Santa Monica, CA, January 1996, pp. 659-667.
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