Work

Twistors-Based Attitude-Orbit Integrated Control for Spacecraft: A High-Order Fully Actuated System Approach

Year: 2024

Type: article

Source: IEEE Transactions on Systems Man and Cybernetics Systems

DOI: 10.1109/tsmc.2024.3519436

Authors: Dongyan Jin, Yannan Bi, Tong Wang, Jianbin Qiu, Huijun Gao

Institution: Harbin Institute of Technology

Language: English

Topic: Spacecraft Dynamics and Control

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funders: National Natural Science Foundation of China, Natural Science Foundation of Hebei Province

Awards: G218475884, G3799234178, G678177963, G684394213

OpenAlex ID: W4405934037

FWCI: 9.238

Cites: 37

Cited by: 52

Related to: 10