Switching Control for Micro Flapping Flight Position in Longitudinal Plane

摘要：

Based on the quasi-state aerodynamic model of micro flapping flight, this paper investigates the aerodynamic lift and drag, and presents a dynamic model in longitudinal plane. Considering the nonlinear and coupled characteristic of micro flapping flight, switching control strategy is used for position control. Then, flapping plane angle and maximal flap angle are chosen as control parameters, according to two kinds of feedback information, switching control law for the micro flapping flight is designed. Finally, climbing flight and horizontal flight of micro flapping flight are simulated. The simulation result suggests that according to the feedback information of the linear combination of position errors and velocity errors, the switching control law is effective, and micro flapping flight moves along the desired trajectory.

作者: Xijin ZHANG Zongde FANG Xiaohui YANG Lan LIU

作者单位: School of Electromechanics Engineering, Northwestern Polytechnical University Xian, Shannxi Province, China

会议类型: 国际会议

会议名称: 第六届中国国际丝绸会议暨第二届国际纺织高层论坛(The 6th China International Silk Conference and The 2nd International Textile Forum)

会议地点: 苏州

会议语种:英文

页码: 201-205

在线出版日期: 2007-09-13（万方平台首次上网日期，不代表论文的发表时间）