Coupled Structure Vibration–Attitude Dynamics Evolution and Control of China’s Space Station
- 8 Downloads
In this paper, a dynamics equation for Spacecraft has first been created using vector mechanics. Second, several attitude dynamics equations of spacecraft have been deduced. Third, a simulation of the coupled structure vibration–attitude dynamics evolution of China Space Station has been researched. Simulation results reveal the generating mechanism and evolutive law of the coupled structure vibration–attitude dynamics of spacecraft. Finally, a simplified experimental platform has been set up, and the experimental results verify the structure vibration–attitude dynamics evolution of the spacecraft and proposed experimental setup.
KeywordsSpacecraft Evolution China Space Station Coupled structure vibration–attitude dynamics
This project is supported by National Natural Science Foundation of China (Grant no. 51605308) “Co-evolution of fractional order coupled structure vibration–attitude dynamic and control of spacecraft”; The Liaoning Province doctor Science Research Fund Project “Co-evolution of fractional order coupled structure vibration–attitude dynamic and control of China Space Station”(Grant no. 201601178); The Liaoning Province “13th Five Year Plan” Higher Education Research Fund Project “Teaching quality monitoring system and safeguard mechanism research on Aerospace engineering majors” (Grant no. GHZD160012); The Liaoning Province Department of Education Fund Project “Study of fractional order coupled structure vibration–attitude dynamic and control of spacecraft” (Grant no. L2015414); The Liaoning Province Department of Education Fund Project “Research and practice on specialty of aerospace engineering based on recognition for engineering education”(Grant no. 030201619);“Exploration and Practice of ‘Theory+Interesting+Research’ Innovative Teaching Mode”(Grant no. YJS2014-11); “Reform and Practice of ‘Theory+Interesting+Research’ Innovative Teaching Mode”(Grant no. JG2017011); “Research on Intelligent Integrated Control of Coupling between Space Solar Power Station Structure Vibration and Attitude Control (Grant no. 13YB22)”.
- 1.Yang J, Qu S, Lin J, Liu Z, Cui X, Wang C, Zhang D, Zhou L, Chen G (2015) Research progress of the structure vibration–attitude coordinated control of spacecraft. Intl J Aeronaut Sp Sci 16(4):112–121Google Scholar
- 28.Ayoubi MA, Sendi C (2013) Takagi-Sugeno fuzzy model-based control of spacecraft with flexible appendage. J Astronaut Sci 61:1–21Google Scholar