Work

Modified Pseudostate Method for Three-Body Problem Under Ephemeris Model

Year: 2026

Type: article

Source: Journal of Guidance Control and Dynamics

DOI: 10.2514/1.g009363

Authors: Yue Dong, Haibin Shang, Jizhong Liu, Jucheng Lu

Institutions: Beijing Institute of Technology, China National Space Administration

Language: English

Topic: Spacecraft Dynamics and Control

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funder: National Natural Science Foundation of China

Award: G251390089

OpenAlex ID: W7127047702

FWCI:

Cites: 17

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