2026-10-14T14:09:35Z https://www.scidb.cn/oai

10.57760/sciencedb.07267 2023-02-17T14:48:10Z

2023-02-17 Time node and parameters of flight trajectory optimization from Earth to Titan doi:10.57760/sciencedb.07267 en By selecting a reasonable gravity assist model and taking the probe launched in 2026 as an example, the optimized trajectory of interstellar voyage from Earth to Titan is designed, and the optimized time node and required velocity increment are simulated. deep space exploration; trajectory optimization; gravity assist; Titan Cui Haiying PUBLIC https://creativecommons.org/licenses/by/4.0/ dataset Science Data Bank