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- W2056522519 abstract "The principle of correcting for inertial guidance error by means of star sighting has been successfully incorporated in automatic inertial navigators for aircraft such as the MK-1 guidance system for the SM62A pilotless bomber. The purpose of this paper is to discuss the application of stellar sighting techniques to the augmentation of inertial guidance for ballistic missiles." @default.
- W2056522519 created "2016-06-24" @default.
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- W2056522519 date "1963-01-01" @default.
- W2056522519 modified "2023-09-25" @default.
- W2056522519 title "Stellar Augmented Inertial Guidance for Ballistic Missiles" @default.
- W2056522519 doi "https://doi.org/10.1109/tme.1963.4323036" @default.
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