Controlled Dynamic System Modeling Experiment
摘要
Establishing the controlled dynamic model of a micro-small fixed-wing Unmanned Aerial Vehicle (UAV) is fundamental. In order to describe the attitude and position of the micro-small fixed-wing UAV, appropriate coordinate systems must be established. The attitude of the fixed-wing UAV in space is mainly described by the rotation relationship among the ground coordinate system, the body coordinate system, the wind coordinate system, and the flight path coordinate system.