Modeling and Optimization of Trans-lunar Orbit for Lunar Polar Station

Lunar polar station is one of the effective ways for private lunar tourism and lunar surface global access mission in the future, the station resupply mission requires a modeling and optimization method for a two-impulse trans-lunar orbit with high-precision dynamics model. It established a model of...

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Main Author: HE Boyong
Format: Article
Language:zho
Published: Editorial Office of Control and Information Technology 2019-01-01
Series:Kongzhi Yu Xinxi Jishu
Subjects:
Online Access:http://ctet.csrzic.com/thesisDetails#10.13889/j.issn.2096-5427.2019.04.011
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author HE Boyong
author_facet HE Boyong
author_sort HE Boyong
collection DOAJ
description Lunar polar station is one of the effective ways for private lunar tourism and lunar surface global access mission in the future, the station resupply mission requires a modeling and optimization method for a two-impulse trans-lunar orbit with high-precision dynamics model. It established a model of fast designing a two-impulse trans-lunar orbit by backward numerical integration, proposed an optimal framework which can be calculated by general nonlinear programming algorithm for solving the trans-lunar orbit and used a golden section strategy to calculate the optimal-fuel solution. Characteristic relationship between the perilune position for braking into a low circular lunar orbit and the duration of transfer was analyzed, and the simulation results demonstrated the validity of the proposed method.
format Article
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institution Kabale University
issn 2096-5427
language zho
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publisher Editorial Office of Control and Information Technology
record_format Article
series Kongzhi Yu Xinxi Jishu
spelling doaj-art-5250b899ff384fd0b6a0eba810e35d1e2025-08-25T06:54:57ZzhoEditorial Office of Control and Information TechnologyKongzhi Yu Xinxi Jishu2096-54272019-01-0136656982330033Modeling and Optimization of Trans-lunar Orbit for Lunar Polar StationHE BoyongLunar polar station is one of the effective ways for private lunar tourism and lunar surface global access mission in the future, the station resupply mission requires a modeling and optimization method for a two-impulse trans-lunar orbit with high-precision dynamics model. It established a model of fast designing a two-impulse trans-lunar orbit by backward numerical integration, proposed an optimal framework which can be calculated by general nonlinear programming algorithm for solving the trans-lunar orbit and used a golden section strategy to calculate the optimal-fuel solution. Characteristic relationship between the perilune position for braking into a low circular lunar orbit and the duration of transfer was analyzed, and the simulation results demonstrated the validity of the proposed method.http://ctet.csrzic.com/thesisDetails#10.13889/j.issn.2096-5427.2019.04.011trajectory optimizationlunar polar stationtrans-lunar orbitreverse numerical integrationsequential quadratic programming(SQP)fast iterative algorithmoptimal-fuel solution
spellingShingle HE Boyong
Modeling and Optimization of Trans-lunar Orbit for Lunar Polar Station
Kongzhi Yu Xinxi Jishu
trajectory optimization
lunar polar station
trans-lunar orbit
reverse numerical integration
sequential quadratic programming(SQP)
fast iterative algorithm
optimal-fuel solution
title Modeling and Optimization of Trans-lunar Orbit for Lunar Polar Station
title_full Modeling and Optimization of Trans-lunar Orbit for Lunar Polar Station
title_fullStr Modeling and Optimization of Trans-lunar Orbit for Lunar Polar Station
title_full_unstemmed Modeling and Optimization of Trans-lunar Orbit for Lunar Polar Station
title_short Modeling and Optimization of Trans-lunar Orbit for Lunar Polar Station
title_sort modeling and optimization of trans lunar orbit for lunar polar station
topic trajectory optimization
lunar polar station
trans-lunar orbit
reverse numerical integration
sequential quadratic programming(SQP)
fast iterative algorithm
optimal-fuel solution
url http://ctet.csrzic.com/thesisDetails#10.13889/j.issn.2096-5427.2019.04.011
work_keys_str_mv AT heboyong modelingandoptimizationoftranslunarorbitforlunarpolarstation