Volume 33 Issue 4
Jul.  2013
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QIAN Hang, ZHENG Jianhua, YU Xizheng, GAO Dong. Dynamics and Control of Displaced Orbits for Solar Sail Spacecraft[J]. Chinese Journal of Space Science, 2013, 33(4): 458-464. doi: 10.11728/cjss2013.04.458
Citation: QIAN Hang, ZHENG Jianhua, YU Xizheng, GAO Dong. Dynamics and Control of Displaced Orbits for Solar Sail Spacecraft[J]. Chinese Journal of Space Science, 2013, 33(4): 458-464. doi: 10.11728/cjss2013.04.458

Dynamics and Control of Displaced Orbits for Solar Sail Spacecraft

doi: 10.11728/cjss2013.04.458
  • Received Date: 2012-09-21
  • Rev Recd Date: 2013-03-08
  • Publish Date: 2013-07-15
  • Based on the linear dynamics model and nonlinear dynamics model, the sun-centred displaced orbits keeping control problem is studied. Firstly, the solar sail dynamics model in cylindrical coordinate form is derived and orbit controllability of the state equation by linearizing the model along the nominal orbit is investigated. Then, by choosing the control weighted matrix R reasonably, a control law for the linear model is designed using the Linear-Quadratic Regulation (LQR) approach. The numerical simulations which are obtained by taking the control law into the nonlinear model indicate that the designed controller which has asymptotic stability and high control accuracy is capable.

     

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