期刊文献+

Design of Station Keeping Mode for Attitude Orbit Control Subsystem of T-SAT

Design of Station Keeping Mode for Attitude Orbit Control Subsystem of T-SAT
下载PDF
导出
摘要 Station keeping mode (SKM) for Attitude Orbit Control Subsystem (AOCS); it is an operational approach regarding the attitude dynamics control. The essential features of the design methodology is researching the basic theory and then afterwards, make an iterative design approach using some premise/assumptions, implementing the system simulation through the Simulink Matlab software package, designing the required controllers, monitor and analyzing the responses until the design give the best results within the range required. Firstly the thruster configuration is designed to acquire the parameters of the torque on the satellite. Next, the controllers are based on the well known PID control law. Controllers optimize the attitude and are used during the maneuvers for SKM. Afterwards the simulation results are given, and presented to demonstrate the performance and validity of the AOCS design approach. Finally the simulation results demonstrate that all the requirements were accomplished and the Station Keeping Mode was successfully designed. Station keeping mode (SKM) for Attitude Orbit Control Subsystem (AOCS); it is an operational approach regarding the attitude dynamics control. The essential features of the design methodology is researching the basic theory and then afterwards, make an iterative design approach using some premise/assumptions, implementing the system simulation through the Simulink Matlab software package, designing the required controllers, monitor and analyzing the responses until the design give the best results within the range required. Firstly the thruster configuration is designed to acquire the parameters of the torque on the satellite. Next, the controllers are based on the well known PID control law. Controllers optimize the attitude and are used during the maneuvers for SKM. Afterwards the simulation results are given, and presented to demonstrate the performance and validity of the AOCS design approach. Finally the simulation results demonstrate that all the requirements were accomplished and the Station Keeping Mode was successfully designed.
出处 《Computer Aided Drafting,Design and Manufacturing》 2010年第2期78-84,共7页 计算机辅助绘图设计与制造(英文版)
关键词 communication satellite AOCS East/West station keeping communication satellite AOCS East/West station keeping
  • 相关文献

参考文献6

  • 1Hoecherl F,Wilke M,Quirmbach O, et al.A toolset for model based AOCS-design. http://interna- tionalisation.ewi.tudelft.nl/live/binaries/...543b.../paper10. pdf .
  • 2Marcel J Sidi.Spacecraft dynamics and control (practical engineering approach)[]..2000
  • 3Wertz J R.Spacecraft attitude determination and control[]..1980
  • 4PETER C.H.Spacecraft Attitude Dynamics[]..2004
  • 5Juergen Schlutz.Attitude and Orbit Control of Small Satellites using Thruster System[]..2005
  • 6Vladimir A C.Spacecraft attitude dynamics and control[]..1991

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部