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NASA NTRS · 19660042499

A technique for optimal final value control of powered flight trajectories.

Pfeiffer, C. G.

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Abstract

Technique for controlling acceleration vector along powered flight trajectory, using linear perturbation method

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Pfeiffer, C. G.. 1966-02-01. A technique for optimal final value control of powered flight trajectories.. https://ntrs.nasa.gov/citations/19660042499

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