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- W2031726143 abstract "Abstract The complete error equations are derived for an inertial navigator operating in a vehicle flying in an arbitrary elliptical orbit. The derivation incorporates a new notation that makes it easy to obtain the basic results in a correct manner. It is shown that the error equations of any inertial navigator (either on earth or in orbit) are identical to the equations for the perturbations of the coordinates of a satellite. When the normalized orbital error equations are coordinatized in a locally level reference frame, they become the Tschauner-Hempel equations. The structure of the solutions of the Tschauner-Hempel equations is discussed in detail, and a partially closed form (sampled data solution) for the case of periodic error sources is presented. A number of typical solutions for various error sources are given, and the problem of reducing these errors by various modes of operation is discussed." @default.
- W2031726143 created "2016-06-24" @default.
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- W2031726143 date "1966-01-01" @default.
- W2031726143 modified "2023-09-27" @default.
- W2031726143 title "Error Equations of Inertial Navigation with Special Application to Orbital Determination and Guidance" @default.
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- W2031726143 doi "https://doi.org/10.1016/b978-1-4832-2729-0.50018-1" @default.
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