NASA NTRS · 19690037512
Iterative guidance applied to generalized missions.
Abstract
Iterative guidance mode /IGM/ applied to effective gravity vector prediction, acceleration measurement of noise sensistivity and energy limitations
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Buckelew, V. L., Chandler, D. C., Horn, H. J.. 1969-01-01. Iterative guidance applied to generalized missions.. https://ntrs.nasa.gov/citations/19690037512
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