Work

Multi-revolution low-thrust trajectory optimization using symplectic methods

Year: 2019

Type: article

Source: Science China Technological Sciences

DOI: 10.1007/s11431-019-9511-7

Authors: ZhiBo E, Davide Guzzetti

Institutions: Tsinghua University, Auburn University

Language: English

Topic: Spacecraft Dynamics and Control

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: green

OpenAlex ID: W2908758132

FWCI: 0.914

Cites: 39

Cited by: 13

Related to: 10