期刊文献+

基于模型的有限预测逆跟踪控制

Finite prediction inversion following control based on model
原文传递
导出
摘要 针对水下无人潜航器(unmanned underwater vehicle,UUV)非最小相位的特性,提出利用有限预测逆方法实现其精确的跟踪控制.利用系统逆方法计算当前时刻t_c的有界的逆输入,需要已知所有未来时刻的理想输出信息.为了有效利用未来时刻的理想输出数据,并提高计算效率,提出将时间窗内理想输出的预测信息用于逆算法中,来求取控制输入值,从而实现对UUV的路径跟踪控制.有限预测逆方法是利用从当前时刻到未来T_p时刻内的理想路径来获得逆输入,可以实现在线控制.通过给定的精确逆输入与利用有限预测逆方法所求得的输入之间的误差,对参数T_p和m进行优化.通过实验验证了该方法的有效性,并对比说明了跟踪误差与优化参数T_p之间的呈指数递减的关系. Considering the non-minimum phase characteristics for unmanned underwater vehicle(UUV),a finite prediction inversion algorithm was proposed to implement the exact following control.The bounded inversion input at current instant t_c was calculated using system inversion method,and the desired output information at future instants must be known.In order to utilize the desired output data effectively and improve the calculating efficiency,the predictive information of desired output in the time window was introduced into the algorithm to obtain the control inputs,and the path following control would be implemented for UUV.The finite predictive inversion method was to introduce the desired path from current instant to future instant T_p to obtain inputs and to complete the real-time computation.Through the error of exact inversion inputs and inputs solved using finite predictive inversion method,the parameters T_p and m were optimized.Simulations are implemented to verify the viability of the algorithm proposed.The contrast simulations with different T_p clarify following error is exponentially decayed with the parameters Tp.
出处 《系统工程理论与实践》 EI CSSCI CSCD 北大核心 2015年第5期1351-1360,共10页 Systems Engineering-Theory & Practice
基金 国家自然科学基金(51179038) 教育部新世纪优秀人才支持计划(NCET-10-0053)
关键词 水下无人潜航器 非最小相位系统 路径跟踪 有限预测逆 unmanned underwater vehicle non-minimum phase system path following finite prediction inversion
  • 相关文献

参考文献10

  • 1王建刚,董新民,薛建平.基于稳定逆的飞机纵向自动着陆控制律设计[J].飞行力学,2011,29(2):33-36. 被引量:2
  • 2陈祥都,刘树堂.用Picard迭代法解约束绳索动点坐标的数学说明[J].东北电力学院学报,1996,16(2):46-55. 被引量:6
  • 3Lionel Lapierre,Didik Soetanto.Nonlinear path-following control of an AUV[J]. Ocean Engineering . 2007 (11)
  • 4Qingze Zou,Santosh Devasia.Precision preview-based stable-inversion for nonlinear nonminimum-phase systems: The VTOL example[J]. Automatica . 2006 (1)
  • 5L.R. Hunt,George Meyer.Stable inversion for nonlinear systems[J]. Automatica . 1997 (8)
  • 6Philippe Martin,Santosh Devasia,Brad Paden.A different look at output tracking: control of a vtol aircraft[J]. Automatica . 1995 (1)
  • 7Devasia, S.,Paden, B.Stable inversion for nonlinear nonminimum-phase time-varying systems. IEEE Transactions on Automatic Control . 1998
  • 8Devasia S,Chen D,Paden B.Nonlinear inversion-based output tracking. IEEE Transactions on Automatic Control . 1996
  • 9Verma A.Determination and stable tracking of feasible aircraft trajectories using adaptive inverse dynamics. . 2000
  • 10Song L.Numercial methods for stable inversion of non-linear systems. . 2002

二级参考文献7

  • 1车军,张新国.自动着陆精确轨迹跟踪控制[J].北京航空航天大学学报,2005,31(9):975-979. 被引量:15
  • 2Qingze Zou,Santosh Devasia. Preview-based stable-inversion for output tracking [ C ]//American Control Conference, Proceedings of the 1999. San Diego, 1999: 3544-3547.
  • 3Qingze Zou, Santosh Devasia. Preview-based stable-inversion for nonlinear nonminimum-phase aircraft tracking: VTOL example [ C ]//AIAA, Guidance, Navigation, and Control Conference and Exhibit. Keystone, Colorado, 2006: 1-4.
  • 4Qingze Zou. Preview-based system-inversion for outputtracking: theory & application [ D ]. USA: University of Washington, 2003.
  • 5Lambregts A A, Creedon J F. Development and flight evaluation of automatic flare laws with improved touchdown dispersion [ R ]. AIAA-80-1757,1980.
  • 6Lambregts A A. Avoiding the pitfalls in automatic control system design [ R ]. Seattle, Washington : Boeing Commer- ci~ Airplane Company, 1982.
  • 7国防科学技术工业委员会.GJB2191-94有人驾驶飞机飞行控制系统通用规范[s].北京:国防科学技术工业委员会,1995.

共引文献8

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