%0 Journal Article %T Second order sliding mode control with backstepping approach for moving mass spinning missiles<br>Second order sliding mode control with backstepping approach for moving mass spinning missiles %A 郭鹏飞 %A 杨树兴 %A 赵良玉 %J 北京理工大学学报(自然科学中文版) %D 2016 %R 10.15918/j.jbit1004-0579.201625.0103 %X 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.<br>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. %K spinning missile moving mass backstepping second order sliding mode control< %K br> %K spinning missile moving mass backstepping second order sliding mode control %U http://journal.bit.edu.cn/yw/bjlgyw/ch/reader/view_abstract.aspx?file_no=20160103&flag=1