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contributor authorZhijun Chen
contributor authorJiaxiang Luo
contributor authorQuan Chen
contributor authorYong Zhao
contributor authorYuzhu Bai
contributor authorXiaoqian Chen
date accessioned2023-11-27T23:05:17Z
date available2023-11-27T23:05:17Z
date issued8/28/2023 12:00:00 AM
date issued2023-08-28
identifier otherJAEEEZ.ASENG-4876.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4293277
description abstractThis study investigated the time-optimal low-thrust interplanetary transfer problem, and proposes a fast estimation method for guessing the initial costate and optimal transfer time based on a surrogate model, and applied it to the problem of the 11th Global Trajectory Optimization Competition (GTOC 11). Two core methods are proposed in this paper: (1) a fast generation method called the neighbor point iteration algorithm (NPIA) is presented for rapidly generating low-thrust databases with high efficiency and accuracy; and (2) deep neural networks (DNNs) are adopted to learn the state–costate pairs of low-thrust databases, and the surrogate network can quickly estimate the initial costate and optimal transfer time of the low-thrust interplanetary problem. Experiments verified the proposed method and investigated the influence of network structure, learning rate, and loss function on the accuracy of network estimation. The effects of database generation and network estimation were compared based on three transfer scenarios: coplanar, non-coplanar, and arbitrary orbital transfer. In addition, the application case study showed that the proposed method can quickly obtain the time-optimal low-thrust solution to GTOC 11’s interplanetary transfer, which achieves high precision and meets the terminal constraints.
publisherASCE
titleFast Estimation of Initial Costate for Time-Optimal Trajectory Based on Surrogate Model
typeJournal Article
journal volume36
journal issue6
journal titleJournal of Aerospace Engineering
identifier doi10.1061/JAEEEZ.ASENG-4876
journal fristpage04023078-1
journal lastpage04023078-13
page13
treeJournal of Aerospace Engineering:;2023:;Volume ( 036 ):;issue: 006
contenttypeFulltext


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