采用理论研究与工程实践相结合的方法,重点研究具有动力学特性的飞机CGF沿航线自主飞行的控制算法,主要包括协调转弯和倾斜转弯控制算法两种,最后以具体航线为例进行测试。结果表明,飞机CGF能够顺利完成飞行任务。 Based on the combination of theoretical research and engineering practice, this paper focuses on the control algorithm of autonomous flight of aircraft CGF along the route with dynamic characteristics, including two kinds of coordinated turn and pitch turn control algorithms. Finally, the specific route is taken as an example to test. The results show that the aircraft CGF can successfully complete the mission.