Design of Optimal Control for a Stratospheric Airship Based on Generalized Coordinate Frame

摘要：

　　An optimal control is presented in this paper.First,nonlinear dynamic model of a six degree of freedom stratospheric airship,traditional and full-actuated,is built based on generalized coordinate frame.Second,optimal control law is determined by Hamilton function and performance index function.This optimal control can be regarded as extension of feedback linearization control law.

关键词： optimal control stratospheric airship generalized coordinate frame

作者: Ming Zhu Yongmei Wu Zewei Zheng

作者单位: School of Aeronautical Science and Engineering,Beihang University,China School of Automation Science and Electrical Engineering,Beihang University,China

会议类型: 国际会议

会议名称: 2012 International Conference on Intelligent System and Applied Material(2012智能系统与应用材料国际会议)(GSAM2012)

会议地点: 太原

会议语种:英文

页码: 587-591

在线出版日期: 2012-01-13（万方平台首次上网日期，不代表论文的发表时间）