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Online Multiphase Reentry Trajectory Optimization for Reusable Rocket based on Intelligent Phase-Transition

Year: 2025

Type: preprint

Source: SSRN Electronic Journal

DOI: 10.2139/ssrn.5412587

Authors: Hongyu Zhou, wang minzhao, Gan Qingzhong, Xiaogang Wang, Cui Naigang

Institutions: Harbin Institute of Technology, China Aerospace Science and Technology Corporation

Language: English

Topic: Spacecraft Dynamics and Control

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: green

OpenAlex ID: W4413776301

Cites: 29

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Related to: 10