Attitude dynamics simulation and analysis of a flexible satellite
Year: 2024
Type: conference-paper
Abstract: Dynamic models of flexible satellites are carried out using the virtual work principle. The kinematic model and the dynamic model are established respectively. The coupling characteristics of the flexible mechanism and its influence on the attitude of the satellite are analyzed by simulation, and the correctness of the mathematical modeling is validated.
Language: English
Subfield: Control and Systems Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: diamond
OpenAlex ID: W4401738752
