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NASA NTRS · 19670024054

Trajectory optimization by steepest ascent method

Cunningham, E. P.

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Abstract

Steepest ascent method for trajectory optimization based on minimum time and maximum velocity of fuel flow rate

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STEEPEST ASCENT METHOD TRAJECTORY OPTIMIZATION FUEL FLOW

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Cunningham, E. P.. 1967-03-01. Trajectory optimization by steepest ascent method. https://ntrs.nasa.gov/citations/19670024054

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