Optimal low-thrust GTO–GSO transfers using differential evolution

被引：0
|
作者：
Padmanabha Prasanna Simha
R V Ramanan
机构：
[1] Vikram Sarabhai Space Centre,
[2] Indian Institute of Space Science and Technology,undefined
来源：
Sādhanā | 2021年 / 46卷
关键词：
Low thrust; trajectory optimization; differential evolution;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Transfers from geosynchronous transfer orbits (GTO) to geosynchronous orbits (GSO) using electric propulsion have been optimized in the current study. Both time-optimal and fuel-optimal trajectories are generated. Three-dimensional equations of motion are considered for the system dynamics. The indirect approach based on optimal control theory is followed and the resulting two-point boundary value problem is solved using differential evolution, a search-based global optimization technique. Optimal trajectories for various mission scenarios are obtained using differential evolution and compared to transfers presented in literature.
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