Work

Simplified optimization model for low-thrust perturbed rendezvous between low-eccentricity orbits

Year: 2023

Type: article

Source: Advances in Space Research

DOI: 10.1016/j.asr.2023.01.016

Authors: An-Yi Huang, Heng-Nian Li

Language: English

Topic: Spacecraft Dynamics and Control

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: green

Funder: National Natural Science Foundation of China

Awards: G3082346921, G4272536896

OpenAlex ID: W4315642014

FWCI: 0.728

Cites: 29

Cited by: 6

Related to: 10