Two direct low thrust trajectory optimization techniques

DOI10.1134/S1064230718060114zbMATH Open1422.90056OpenAlexW2916577559WikidataQ128383929 ScholiaQ128383929MaRDI QIDQ2320308

A. A. Tselousova, S. P. Trofimov, M. G. Shirobokov

Publication date: 22 August 2019

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s1064230718060114

zbMATH Keywords

impulses approximatingthrust acceleration

Mathematics Subject Classification ID

Applications of mathematical programming (90C90) Nonlinear programming (90C30)

Cites Work

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• Complete closed-form solutions of the Stark problem
• \(F\) and \(G\) Taylor series solutions to the Stark and Kepler problems with Sundman transformations
• Direct trajectory optimization using nonlinear programming and collocation

Related Items (2)

A simple targeting technique for two-body spacecraft trajectories ⋮ Flatness-Based Low-Thrust Trajectory Optimization for Spacecraft Proximity Operations

Uses Software

• Title not available (Why is that?)
• OTIS

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