[136]HESSE H, PALACIOS R. Reduced-order aeroelastic models for dynamics of maneuvering flexible aircraft[J]. AIAA Journal, 2014, 52(8): 1717. DOI: 10.2514/1.J052684
[137]LIVNE E. Aircraft active flutter suppression: State of the art and technology maturation needs[J]. Journal of Aircraft, 2018, 55(1): 410. DOI: 10.2514/1.C034442
[138]MUKHOPADHYAY V. Historical perspective on analysis and control of aeroelastic responses[J]. Journal of Guidance, Control, and Dynamics, 2003, 26(5): 673. DOI: 10.2514/2.5108
[139]LIVNE E. Future of airplane aeroelasticity[J]. Journal of Aircraft, 2003, 40(6): 1066. DOI: 10.2514/2.7218
[140]LEE K W, SINGH S N. Adaptive control of multi-input aeroelastic system with constrained inputs[J]. Journal of Guidance, Control, and Dynamics, 2015, 38(12): 2337. DOI: 10.2514/1.G001022
[141]NGUYEN N T, SWEI S M, TING E. Adaptive linear quadratic gaussian optimal control modification for flutter suppression of adaptive wing[C]//Proceedings of the AIAA Infotech @ Aerospace. Kissimmee, Florida: AIAA, 2015: 1. DOI: 10.2514/6.2015-0118
[142]DANOWSKY B P, THOMPSON P M, LEE D C, et al. Modal isolation and damping for adaptive aeroservoelastic suppression[C]//Proceedings of the AIAA Atmospheric Flight Mechanics (AFM) Conference. Boston, MA: AIAA, 2013: 1. DOI: 10.2514/6.2013-4743
[143]CESNIK C E S, ORTEGA-MORALES M. Active aeroelastic tailoring of slender flexible wings[C]//Proceedings of the International Forum on Aeroelasticity and Structural Dynamics. Madrid, Spain: Council of European Aerospace Societies, 2001: 497
[144]AFONSO F, VALE J, OLIVEIRA E, et al. Active flutter suppression of a high aspect-ratio wing using aileron control[C]//Proceedings of the 6th EASN International Conference on Innovation in European Aeronautics Research, Porto, Portugal: [s.n.], 2016
[145]ZHAO Zhenjun, REN Gexue. Multibody dynamic approach of flight dynamics and nonlinear aeroelasticity of flexible aircraft[J]. AIAA Journal, 2011, 49(1): 41. DOI: 10.2514/1.45334
[146]DILLSAVER M J, CESNIK C E S, KOLMANOVSKY I V. Gust load alleviation control for very flexible aircraft[C]//Proceedings of the AIAA Atmospheric Flight Mechanics Conference. Portland, Oregon: AIAA, 2011: 1. DOI: 10.2514 /6.2011-6368
