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NASA NTRS · 20160008235

Partial Derivatives of the Lambert Problem

Abstract

A procedure for deriving analytic partial derivatives of the Lambert problem is presented. Using the universal, cosine based Lambert formulation; first order partial derivatives of the velocities with respect to the positions and times are developed. Taking advantage of inherent symmetries and intermediate variables, the derivatives are expressed in a computationally efficient form. The added cost of computing these partials is found to be approximately 10% to approximately 60% of the Lambert compute cost. The availability of analytic partial derivatives increases optimization speed, efficiency and allows for trajectory optimization formulations that implicitly enforce continuity constraints via embedded Lambert problems.

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BibTeXRIS

Arora, Nitin, Russell, Ryan P., Strange, Nathan. 2014-08-05. Partial Derivatives of the Lambert Problem. https://ntrs.nasa.gov/citations/20160008235

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