Tang Liang, Roemer M, Ge Jianhua.Methodologies for adaptive flight envelope estimation and protection[C]//AIAA Guidance, Navigation, and Control Conference.Chicago, Illinois:, 2009:1-14
[2]
Bacon B J, Gregory I M.General equations of motion for a damaged asymmetric aircraft[C]//AIAA Atmospheric Flight Mechanics Conference and Exhibit.Hilton Head, South Carolina:, 2007:1-13
[3]
Goman M G, Khramtsovsky A V, Kolesnikov E N.Evaluation of aircraft performance and maneuverability by computation of attainable equilibrium sets[J].Journal of Guidance, Control, and Dynamics, 2008, 31 (2):329-339
[4]
Shah G H.Aerodynamic effects and modeling of damage to transport aircraft[C]//AIAA Atmospheric Flight Mechanics Conference and Exhibit.Honolulu, Hawai:, 2008:1-13
[5]
Pandita R, Chakraborty A, Seiler P.Reachability and region of attraction analysis applied to GTM dynamic flight envelope assessment[C]//AIAA Guidance, Navigation, and Control Conference.Chicago, Illinois:, 2009:1-21
[6]
Urnes J M, Reichenbach E Y Sr, Smith T A.Dynamic flight envelope assessment and prediction[C]//AIAA Guidance, Navigation and Control Conference and Exhibit.Honolulu, Hawaii:, 2008:1-10
[7]
Keller1 J D, McKillip R M, JrKim S.Aircraft flight envelope determination using upset detection and physical modeling methods[C]//AIAA Guidance, Navigation, and Control Conference.Chicago, Illinois:, 2009, 1-21
[8]
Tang Liang, Roemer M, Bharadwaj S.An integrated health assessment and fault contingency management system for aircraft[C]//AIAA Guidance, Navigation and Control Conference and Exhibit.Honolulu, Hawaii:, 2008:1-9
[9]
Moncayo H, Perhinschi M G, Davis J.Artificial-immune-system-based aircraft failure evaluation over extended flight envelope[J].Journal of Guidance, Control, and Dynamics, 2011, 34 (4):989-1002
[10]
Tang Liang, Roemer M, Ge Jianhua.Methodologies for adaptive flight envelope estimation and protection[C]//AIAA Guidance, Navigation, and Control Conference.Chicago, Illinois:, 2009:1-14
[11]
Morelli E A, Smith M S.Real-time dynamic modeling-data information requirements and flight test results[C]//AIAA Atmospheric Flight Mechanics Conference and Exhibit.2008
[12]
黄成涛, 王立新.多操纵面飞翼构型飞机舵面故障在线诊断方法[J].航空学报, 2011, 32 (1):58-66 Huang Chengtao, Wang Lixin.On-line fault diagnosis for control surface of multi-control effector flying wings[J].Acta Aeronautica et Astronautica Sinica, 2011, 32 (1):58-66 (in Chinese)
[13]
Goman M G, Khramtsovsky A V, Kolesnikov E N.Evaluation of aircraft performance and maneuverability by computation of attainable equilibrium sets[J].Journal of Guidance, Control, and Dynamics, 2008, 31 (2):329-339
[14]
方振平.飞机飞行动力学[M].北京:北京航空航天大学出版社, 2008:25-45 Fang Zhenping.Aircraft flight dynamic[M].Beijing:Beijing University of Aeronautics and Astronautics Press, 2008:25-45 (in Chinese)
[15]
Pandita R, Chakraborty A, Seiler P.Reachability and region of attraction analysis applied to GTM dynamic flight envelope assessment[C]//AIAA Guidance, Navigation, and Control Conference.Chicago, Illinois:, 2009:1-21
[16]
Keller1 J D, McKillip R M, JrKim S.Aircraft flight envelope determination using upset detection and physical modeling methods[C]//AIAA Guidance, Navigation, and Control Conference.Chicago, Illinois:, 2009, 1-21
[17]
Moncayo H, Perhinschi M G, Davis J.Artificial-immune-system-based aircraft failure evaluation over extended flight envelope[J].Journal of Guidance, Control, and Dynamics, 2011, 34 (4):989-1002
[18]
Morelli E A, Smith M S.Real-time dynamic modeling-data information requirements and flight test results[C]//AIAA Atmospheric Flight Mechanics Conference and Exhibit.2008
[19]
黄成涛, 王立新.多操纵面飞翼构型飞机舵面故障在线诊断方法[J].航空学报, 2011, 32 (1):58-66 Huang Chengtao, Wang Lixin.On-line fault diagnosis for control surface of multi-control effector flying wings[J].Acta Aeronautica et Astronautica Sinica, 2011, 32 (1):58-66 (in Chinese)
[20]
方振平.飞机飞行动力学[M].北京:北京航空航天大学出版社, 2008:25-45 Fang Zhenping.Aircraft flight dynamic[M].Beijing:Beijing University of Aeronautics and Astronautics Press, 2008:25-45 (in Chinese)
