New Analytic Solution with Continuous Thrust: Generalized Logarithmic Spirals
Author:
Affiliation:
1. Technical University of Madrid, Madrid E-28040, Spain
2. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109-8099
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.G000341
Reference46 articles.
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3. Shape-Based Algorithm for the Automated Design of Low-Thrust, Gravity Assist Trajectories
4. Design and Optimization of Low-Thrust Trajectories with Gravity Assists
5. VasileM.SchützeO.JungeO.RadiceG.DellnitzM.IzzoD. “Spiral Trajectories in Global Optimisation of Interplanetary and Orbital Transfers,” ESA, Ariadna Study Rept. ID-AO4919 05/4106, Noordwijk, the Netherlands, 2006.
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