[1] Miao Y, Wang X, Miao Y, Wang S. Dynamics and adaptive fault-tolerant flight control under structure damage of horizontal stabilizer. Aerospace Science and Technology. 2020;106:106135. DOI 10.1016/j.ast.2020.106135
[2] Board S. In-Flight Separation of Vertical Stabilizer American Airlines Flight 587 Airbus Industrie A300-605R, N14053 Belle Harbor, New York November 12, 2001. National Transportation Safety Board. 2001;490. DOI NTSB/AAR-04/04
[3] Zhang Y, Jiang J. Bibliographical review on reconfigurable fault-tolerant control systems. Annual reviews in control. 2008;32(2):229-52. DOI 10.1016/j.arcontrol.2008.03.008
[4] Abbaspour A, Mokhtari S, Sargolzaei A, Yen KK. A survey on active fault-tolerant control systems. Electronics. 2020;9(9):1513. DOI 10.3390/electronics9091513
[5] Zhang Y, Huang Y, Chu Q, de Visser CC. Database-driven safe flight-envelope protection for impaired aircraft. Journal of Aerospace Information Systems. 2021;18(1):14-25. DOI 10.2514/1.I010846
[6] Hugo G. Autonomous landing of a fixed-Wing unmanned aircraft with partialwing and stabiliser losses: Stellenbosch: Stellenbosch University; 2017.
[7] Wang J, Wang S, Wang X, Shi C, Tomovic MM. Active fault tolerant control for vertical tail damaged aircraft with dissimilar redundant actuation system. Chinese Journal of Aeronautics. 2016;29(5):1313-25.
[8] Asadi D, Sabze Parvar M, Taalebi H.A, Abbasi H. The Study of Wing Damage Effect on Airplane Performance and Flight Dynamics. Journal of Aeronautical Engineering. 2012;14(2):17-33 (in persian). DOR 20.1001.1.17359449.1391.14.2.3.1
[9] Bacon B, Gregory I, editors. General equations of motion for a damaged asymmetric aircraft. AIAA atmospheric flight mechanics conference and exhibit; 2007. DOI 10.2514/6.2007-6306
[10] Chao D, Qi R, Jiang B, Soh Y. Adaptive fault-tolerant control for ascent HSV with wing damage and function constraints on states. Acta Astronautica. 2024. DOI 10.1016/j.actaastro.2024.06.024
[11] Zhang L, Mu J, Ma H, Dai G, Tong S. Research on fault-tolerant control of combined airframe damage of electric aircraft. Aerospace. 2023;10(7):611. DOI 10.3390/aerospace10070611
[12] Yuwei C, Aijun L, Xianfeng M. A fault-tolerant control method for distributed flight control system facing wing damage. Journal of Systems Engineering and Electronics. 2021;32(5):1041-52. DOI 10.23919/JSEE.2021.000089
[13] Zhang J, Xu X, Yang L, Yang X. LPV model-based multivariable indirect adaptive control of damaged asymmetric aircraft. Journal of Aerospace Engineering. 2019;32(6):04019095. DOI 10.1061/(ASCE)AS.1943-5525.0001089
[14] Ijaz S, Hamayun MT, Yan L, Shi C. Active fault-tolerant control for vertical tail damaged aircraft with dissimilar redundant actuation system using integral sliding mode control. Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science. 2019;233(7):2361-78. DOI 10.1016/j.cja.2016.08.009
[15] Zhang J, Yang X, Yang L. Virtual-command-based model reference adaptive control for abrupt structurally damaged aircraft. Aerospace Scienceand Technology. 2018;78:452-60. DOI 10.1016/j.ast.2018.04.043
[16] Li Y, Liu X, Ming R, Zhu H, Zhang W. A cascaded nonlinear fault-tolerant control for fixed-wing aircraft with wing asymmetric damage. ISA transactions. 2023;136:503-24. DOI 10.1016/j.isatra.2022.10.021
[17] Asadi D, Bagherzadeh SA. Nonlinear adaptive sliding mode tracking control of an airplane with wing damage. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 2017;232(8):1405-20. DOI 10.1177/0954410017690546
[18] Asadi D, Ahmadi K. Nonlinear robust adaptive control of an airplane with structural damage. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 2020;234(14):2076-88. DOI 10.1177/0954410020926618
[19] He Q, Tan Y, Liu X, Jia Q, Liu J. Reconfigurable Nonlinear Dynamic Inversion for Attitude Control of a Structurally Damaged Aircraft. IEEE Access. 2020;8:199931-43.
[20] Ahmadi K, Asadi D, Pazooki F. Nonlinear L1 adaptive control of an airplane with structural damage. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 2019;233(1):341-53. DOI 10.1177/0954410017730088
[21] Roskam J, editor Methods for Estimating Stability and Control Derivatives of Conventional Subsonic Airplanes1971.
[22] Sadati S.H, Menhaj M.B, Sabze Parvar M. Nonlinear adaptive flight control using dynamic inversion and neural networks controller. Amirkabir Journal of Mechanical Engineering. 2007;38(1):18 (in persian). URL https://ajsr.aut.ac.ir/article_2366_2efbed79d6ad9bb9350179d91ac95939.pdf
[23] Radatnia S, Faraji J, Keighobadi J. Design and implementation a novel inertial sensor errors model in extended Kalman filter based on genetic algorithm. Journal of Mechanical Engineering. 2020;50(3):97-106 (in persian). DOI 10.22034/jmeut.2020.9554
[24] Crassidis JL, Junkins JL. Optimal estimation of dynamic systems: Chapman and Hall/CRC; 2004.
[25] Faraji J, Keighobadi J. Design and simulation of the integral backstepping sliding mode control and extended Kalman-Bucy filter for quadrotor. Journal of Mechanical Engineering. 2020;50(4(93)):131-140 (in persian). DOI 10.22034/jmeut.2021.9416
[26] Slotine J-JE, Li W. Applied nonlinear control: Prentice hall Englewood Cliffs, NJ; 1991.
[27] Tol H, De Visser C, Sun L, van Kampen E, Chu Q. Multivariate spline-based adaptive control of high-performance aircraft with aerodynamic uncertainties. Journal of Guidance, Control, and Dynamics. 2016;39(4):781-800. DOI 10.2514/1.G001079
[28] Abbaspour A, Aboutalebi P, Yen KK, Sargolzaei A. Neural adaptive observer-based sensor and actuator fault detection in nonlinear systems: Application in UAV. ISA transactions. 2017;67:317-29. DOI 10.1016/j.isatra.2016.11.005
[29] Lee JD, Kim L, Zewge NS, Bang H. Fault-Tolerant Control for Aircraft with Structural Damage Using Sparse Online Gaussian Process Regression. International Journal of Aeronautical and Space Sciences. 2024:1-25. DOI 10.1007/s42405-024-00715-7
[30] Sadati S.H. Aircraft control augmentation system design usin dynamic inversion and neural network. Journal of Aeronautical Engineering. 2017;18(2):85-97 (in persian). URL 20.1001.1.17359449.1395.18.2.7.3
[31] Roskam J. Airplane flight dynamics and automatic flight controls: DARcorporation; 1998.
[32] Bodson M, Groszkiewicz JE. Multivariable adaptive algorithms for reconfigurable flight control. IEEE transactions on control systems technology. 1997;5(2):217-29. DOI 10.1109/87.556026
[33] Mobini Bidgoli M, Sadati S.H. Flight control using adaptive dynamic inversion. Aerospace Knowledge and Technology Journal. 2016;5(1):7-16 (in persian). URL http://www.astjournal.ir/article_19740_b35ee022d7599d2d75b8f08a9be37f02.pdf
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