Abstract: | The Multi sensor Integrated Navigation System (MINS) is being developed by Litton Guidance and Control as a solution to the ever present problem of providing enhanced accuracy inertial navigation performance at costs generally equated to medium accuracy systems. The MINS is a generalized concept comprised of a medium accuracy Inertial Navigation Unit (INS) that accepts and processes bounding inputs from position and/or velocity sensors singly or in combinations. It is not limited, to a specific application, rather the MINS concept is a viable solution to a variety of diverse system requirements. The first section of this paper discusses the conceptual aspects. Of the MINS. The remainder of the paper concentrates on a specific application to which the MINS concept has been successfully applied. Estimates of. performance derived from simulations for various sensor input configurations will be presented. |
Published in: |
Proceedings of the 1989 National Technical Meeting of The Institute of Navigation January 23 - 26, 1989 San Mateo, CA |
Pages: | 181 - 194 |
Cite this article: | Portney, Joe N., Breslau, Ray W., "Multisensor Integrated Navigation System," Proceedings of the 1989 National Technical Meeting of The Institute of Navigation, San Mateo, CA, January 1989, pp. 181-194. |
Full Paper: |
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