Abstract
The Canadian Helicopter Integrated Navigation System (HINS), designed for an ASW helicopter, is described. The HINS Advanced Development Model is configured with an F-cubed RUG inertiaI navigator, GPS receiver and Doppler velocity sensor, and integrated using multiple Kalman filters and redundancy management algorithms. The system offers high levels of performance, fault tolerance and reliability. Performance characteristics are described, as are possible future developments and applications of the technology.
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© 1989 Springer-Verlag Berlin Heidelberg
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Scherzinger, B.M., Blake Reid, D. (1989). Integration of INS, GPS and Doppler for Helicopter Navigation. In: Linkwitz, K., Hangleiter, U. (eds) High Precision Navigation. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-74585-0_42
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DOI: https://doi.org/10.1007/978-3-642-74585-0_42
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-74587-4
Online ISBN: 978-3-642-74585-0
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