New Analytic Solution with Continuous Thrust: Generalized Logarithmic Spirals

Author:

Roa Javier1,Peláez Jesús1,Senent Juan2

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

Reference46 articles.

1. Logarithmic Spiral: An Ideal Trajectory for the Interplanetary Vehicle with Engines of Low Sustained Thrust

2. Interplanetary Travel by Solar Sail

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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