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NASA NTRS · 19630022697

A TECHNIQUE FOR OPTIMUM FINAL VALUE CONTROL OF POWERED FLIGHT TRAJECTORIES

Pfeiffer, C. G.

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Abstract

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

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TRAJECTORY CONTROL FLIGHT PATH CONTROL OPTIMAL CONTROL

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Pfeiffer, C. G.. 1963-06-20. A TECHNIQUE FOR OPTIMUM FINAL VALUE CONTROL OF POWERED FLIGHT TRAJECTORIES. https://ntrs.nasa.gov/citations/19630022697

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