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Article Navigation> JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY> 2016> 25(1): 17-22
GUO Peng-fei, YANG Shu-xing, ZHAO Liang-yu. Second order sliding mode control with backstepping approach for moving mass spinning missiles[J]. JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2016, 25(1): 17-22. doi: 10.15918/j.jbit1004-0579.201625.0103
Citation: GUO Peng-fei, YANG Shu-xing, ZHAO Liang-yu. Second order sliding mode control with backstepping approach for moving mass spinning missiles[J].JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2016, 25(1): 17-22.doi:10.15918/j.jbit1004-0579.201625.0103
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Second order sliding mode control with backstepping approach for moving mass spinning missiles

doi:10.15918/j.jbit1004-0579.201625.0103

  • School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China

  • Received Date:2014-03-31
    Abstract
  • An attitude controller using the second order sliding mode control methodology with a backstepping approach (SOSMCB) is designed and implemented for a spinning missile with two internal moving mass blocks. The system consists of a rigid body and two radial internal moving mass blocks and its mathematical model is established based on Newtonian mechanics. The control scheme integrates a second order sliding mode control algorithm into the last step of the backstepping approach, and its stability is proved by means of a Lyapunov function. The performance of the controller is demonstrated by numerical simulations, the results show that the attitude controller is stable and effective.
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