On Longitudinal Control of Landing for UAVs under Complex Conditions

LI Lei; HUANG Yi-min; SUN Chun-zhen

doi:10.3969/j.issn.1671-637x.2014.11.012

[1] BROCKHAUS R.Flight control［M］.Beijing：National Defense Industry Press,1999.

[2] ZHU W W.Research on whole envelop control law design technology for automatic takeoff and landing UAV［D］.Nanjing:Nanjing University of Aeronautics and Astronautics,2012.

[3] SONG H.Research on automatic landing control technologies for UAV under complex conditions［D］.Nanjing:Nanjing University of Aeronautics and Astronautics,2011.

[4] WU S T,FEI Y H.Flight control system［M］.Beijing:Beihang University Press,2005.

[5] STEVENS B L,LEWIS F L.Aircraft control and simulation［M］.New York:John Wiley & Sons,Inc.,1993.

[6] HSIAO F B,CHAN W L,LAI Y C,et al.Landing longitudinal control system design for fixed wing UAV［C］//45 th AIAA Aerospace Sciences Meeting and Exhibit 2007,Reno, AIAA 2007-868.

[7] FALEIRO L F,LAMBREGTS A A.Analysis and tuning of a ‘Total Energy Control System’control law using eigenstructure assignment ［J］.Aerospace Science and Technology,1999(3):127-140.

[8] CHE J.Automatic landing control using H∞ control and stable inversion［C］//Proceedings of the 40th IEEE Conference on Decision and Control,Florida,2001:241-246.

[9] OHNO M,YAMAGUCHI Y,HATA T,et al.Robust control law design for an automatic landing flight experiment［J］.Control Engineering Practice,1999,7(9):1143-1151.