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NASA NTRS · 19660027013

Coordinate systems for differential correction

Emerson, E. A.·Lemmon, W. W.

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Abstract

System of state transition partial derivatives for which tracking information normal matrix for lunar orbiter is nearly diagonalized

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STATE EQUATION LUNAR ORBITER ORBITAL CALCULATION TRACKING STUDY

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Emerson, E. A., Lemmon, W. W.. 1966-09-01. Coordinate systems for differential correction. https://ntrs.nasa.gov/citations/19660027013

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