Work

A Fast Solution to Impulse Controllable Set of Direct Abort Orbits From Low Lunar Orbit Based on Deep Learning

Year: 2025

Type: article

Source: IEEE Transactions on Aerospace and Electronic Systems

DOI: 10.1109/taes.2025.3618994

Authors: Zhen-jiang Du, Hai-yang Li, Lin Lu, Bin-yu Zhu, Xiao-tong Bu

Institution: China Astronaut Research and Training Center

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: G7163718393

OpenAlex ID: W7085127616

FWCI: 1.939

Cites: 49

Cited by: 5

Related to: