DocumentCode
1595033
Title
Establishing Stratosail´s 6-DOF Dynamics Models
Author
Supeng Zhu ; Wenxing Fu
Author_Institution
Coll. of Astronaut., Northwestern Polytech. Univ., Xi´an, China
fYear
2012
Firstpage
683
Lastpage
686
Abstract
The stratosail has the tensile force of the tether but no engine thrust and the size and direction of the tensile force is constantly changing. Also the changes in the size and direction of wind speed have direct influence on the aerodynamic force and spatial position of the stratosail. The establishment of the stratosail´s 6-DOF models includes the modeling of a flexible tether, that of the position restriction body and that of the aerodynamic force of the stratosail, thus being a complicated flexible and rigid coupled modeling process. This paper analyzes the forces received by the stratosail and establishes its dynamics model and kinematics model under the stratosail´s coordinate system. The forces include the gravity and aerodynamic force exerted on the stratosail and the tensile force and moment of the tether. According to theoretical mechanics principles, it also establishes the stratosail´s mass center dynamics equation and the dynamics equation rotating around its mass center, laying the foundation for further analysis of the changes in the attitude of the stratosail and in the spatial position of its mass center.
Keywords
aerodynamics; flexible structures; position control; space tethers; tensile strength; 6-DOF dynamics models; aerodynamic force; flexible tether; kinematics model; mass center dynamics equation; position restriction body; spatial position; stratosail; tensile force; Aerodynamics; Earth; Equations; Gravity; Mathematical model; Aerodynamic Force; Coordinate System; Models; Stratosail; Stratospheric Satellite; Tensile Force;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent System Design and Engineering Application (ISDEA), 2012 Second International Conference on
Conference_Location
Sanya, Hainan
Print_ISBN
978-1-4577-2120-5
Type
conf
DOI
10.1109/ISdea.2012.454
Filename
6173298
Link To Document