海军航空工程学院学报
海軍航空工程學院學報
해군항공공정학원학보
JOURNAL OF NAVAL AERONAUTICAL ENGINEERING INSTITUTE
2014年
3期
217-220
,共4页
李振山%陈勇%雷军委
李振山%陳勇%雷軍委
리진산%진용%뢰군위
倒立摆%积分%滑模%非线性%耦合
倒立襬%積分%滑模%非線性%耦閤
도립파%적분%활모%비선성%우합
inverted pendulum%integral%sliding mode%nonlinear%coupling
在研究了倒立摆系统动力学模型的基础上,提出了一种积分滑模变结构的控制方法。通过设计积分性质的非线性滑模面,可以减少系统静差,提高控制精度,系统鲁棒性能获得了很好的保存。仿真证明,该方法能够在较短时间内实现系统的稳定,提高系统的控制精度,使倒立摆系统具有更高的稳定性和鲁棒性。
在研究瞭倒立襬繫統動力學模型的基礎上,提齣瞭一種積分滑模變結構的控製方法。通過設計積分性質的非線性滑模麵,可以減少繫統靜差,提高控製精度,繫統魯棒性能穫得瞭很好的保存。倣真證明,該方法能夠在較短時間內實現繫統的穩定,提高繫統的控製精度,使倒立襬繫統具有更高的穩定性和魯棒性。
재연구료도립파계통동역학모형적기출상,제출료일충적분활모변결구적공제방법。통과설계적분성질적비선성활모면,가이감소계통정차,제고공제정도,계통로봉성능획득료흔호적보존。방진증명,해방법능구재교단시간내실현계통적은정,제고계통적공제정도,사도립파계통구유경고적은정성화로봉성。
Based on the research on the inverted pendulum system dynamics model, a kind of integral sliding mode variable structure control method was proposed in this paper. The static error could be reduced and control precision could be proved by the introducing of integral item. Also the system had a strong robustness as the using of sliding mode control. Fi-nally, a detailed numerical simulation was done and the rightness and robustness of the proposed method was testified.