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Near optimal shuttle trajectories using accelerated gradient methods

I. L. Johnson, James L. Kamm

Open publisher page 10 citations

Abstract

Optimal ascent trajectories for delta wing space shuttle flight, using accelerated gradient methods

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Optimal ascent trajectories for delta wing space shuttle flight, using accelerated gradient methods

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OpenAlex reports 10 citations for this work. Citation counts describe recorded attention and do not establish research quality.

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Available abstract

Optimal ascent trajectories for delta wing space shuttle flight, using accelerated gradient methods

Key concepts: Space Shuttle, Computer science, Engineering, Aerospace engineering

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