电光与控制, 2013, 20 (7): 32, 网络出版: 2013-07-09
微波着陆系统横向自动进近控制律设计
Design of an MLS Lateral Automatic Landing System Control Law
微波着陆 自动着陆 轨迹跟踪 飞行控制 Microwave Landing System (MLS) automatic landing trajectory tracking flight control
摘要
为更好地发挥微波着陆大范围着陆制导的优势,设计了一种新型的微波着陆横向轨迹自动生成控制律,可根据飞机初始位置和姿态生成一条进近轨迹并控制飞机沿此轨迹对准跑道中心线;提出了单圆、S型和直接指数进近3种进近模态,并分别对3种模态设计了控制律。仿真结果表明,所设计的控制律能够指引飞机在不同初始条件下对准跑道。
Abstract
In order to make full use of the advantages of microwave landing system (MLS) on widerange landing guidancean MLS lateral autolanding control law with automatic path definition was designedwhich could generate an approaching trajectory according to the aircrafts initial position and attitude and control the aircraft towards the runway centerline.Three approaching modes were proposed:single circularS shape and direct centerline approaching.The control laws for the three approaching modes were designed.Simulation shows that the control laws can guide the aircraft towards the centerline of runway under different initial conditions.
徐宁, 董新民, 程建锋, 王昱苏. 微波着陆系统横向自动进近控制律设计[J]. 电光与控制, 2013, 20(7): 32. XU Ning, DONG Xinmin, CHENG Jianfeng, WANG Yusu. Design of an MLS Lateral Automatic Landing System Control Law[J]. Electronics Optics & Control, 2013, 20(7): 32.