【作者】 彭良福； 林云松；

【Author】 PENG Liangfu1,LIN Yunsong2 1.College of Electrical Information Engineering,Southwest University for Nationalities,Chengdu 610041,P.R.China 2.College of Automation,University of Electronic Science and Technology of China,Chengdu 610054,P.R.China

【机构】 西南民族大学电气信息工程学院； 电子科技大学自动化工程学院；

【摘要】 利用僚机的实际位置与正确编队位置之间的位置偏差,采用非线性动态逆的方法设计了编队飞行位置误差控制器,给出了基于动态逆的编队飞行位置控制系统的实现方案,并且分别对长机加速,爬升和转向时僚机跟随长机机动飞行的情况进行了计算机仿真.仿真结果表明,这种编队飞行位置控制方法可以使编队飞行的位置误差控制在允许的范围内,实现编队队形的保持。更多还原

【Abstract】 A position error control method for formation flight based on dynamic inversion is provided according to the position error between the wing plane and its correct position in formation.An implementing program of position control system based on dynamic inversion for formation flight is suggested.In order to evaluate the validity of the method,many cases are simulated that the wing plane follows the leader plane when the leader plane speed up,climb up and turn.The computer simulation results indicate that the position error can be reduced in an allowable range of formation flight by this control method,so the formation configuration can be kept.更多还原