Optimal thrust level for orbit insertion-Reference-Cited by-同舟云学术

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Optimal thrust level for orbit insertion

Published:2017-07 Issue: Volume:136 Page:55-63
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Cerf Max

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference53 articles.

1. Optimal Trajectories for Space Navigation;Lawden,1963

2. Optimization Techniques with Applications to Aerospace System;Leitmann,1962

3. Optimal Space Trajectories;Marec,1979

4. Mécanique céleste et contrôle des véhicules spatiaux;Bonnard,2006

5. Fuel-optimal trajectories for aeroassisted coplanar orbital transfer problem;Naidu;IEEE Trans. Aerosp. Electron. Syst.,1990

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1. An integrated optimum 3D transition orbit design procedure with guidance for a spacecraft;Advances in Space Research;2021-10

2. Versatile Launcher Preliminary Design;Journal of Spacecraft and Rockets;2019-03

3. Design, Modeling and Performance Optimization for Propulsion of a Small Launch Vehicle;IOP Conference Series: Materials Science and Engineering;2018-11-29

4. Optimal injection point for launch trajectories with parametric thrust profile;Acta Astronautica;2018-10

5. Fast solution of minimum-time low-thrust transfer with eclipses;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2018-07-18

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