The process and characteristic of landing of transport aircraft was analyzed. The synthesis method based on structured singular value was adopted to design the automatic landing control system to accurately follow the slide path of landing. The robust performance of the landing system was analyzed. The simulation results showed that the designed control law satisfied the requirements of automatic landing of transport aircraft when there are uncertainties of transport aircraft model, measurement noises and gust disturbances.
Wang Hui, Li Shaoyan, Chen Zongji.Design of longitudinal automatic landing control law of transport aircraft with μ synthesis[J] JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2003,V29(12): 1059-1063