Low-Thrust Gravity-Assist Trajectory Design Using Optimal Multimode Propulsion Models
Author:
Affiliation:
1. Texas A&M University, College Station, Texas 77843-3141
2. Auburn University, Auburn, Alabama 36849
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
https://arc.aiaa.org/doi/pdf/10.2514/1.G005750
Reference24 articles.
1. The Dawn Mission to Minor Planets 4 Vesta and 1 Ceres
2. Chang-DiazF. R.BradenE.JohnsonI.HsuM. M.YangT. F. “Rapid Mars Transits with Exhaust-Modulated Plasma Propulsion,” NASA TP 3539, 1995.
3. Optimal low-thrust transfer using variable bounded thrust
4. Optimization of Variable-Specific-Impulse Interplanetary Trajectories
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