[1] Ansari AR, Novinzadeh AR. Designing a control system for an airplane wing flutter employing gas actuators. International Journal of Aerospace Engineering. 2017, 4209619. DOI :10.1155/2017/4209619.
[2] Moosavi R, Elasha F. Smart wing flutter suppression. Designs. 2022;6(2):29. DOI :10.3390/designs6020029.
[3] Ouyang Y, Gu Y, Kou X, Yang Z. Active flutter suppression of wing with morphing flap. Aerospace Science and Technology. 2021;110:106457. DOI :10.1016/j.ast.2020.106457.
[4] Ghasemikaram AH, Mazidi A, Fazel MR, Fazelzadeh SA. Flutter suppression of an aircraft wing with a flexibly mounted mass using magneto-rheological damper. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 2020;234(3):827-39. DOI :10.1177/0954410019887039.
[5] De Breuker R, Abdalla M, Milanese A, Marzocca P. Optimal control of aeroelastic systems using synthetic jet actuators. In49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 16th AIAA/ASME/AHS Adaptive Structures Conference, 10th AIAA Non-Deterministic Approaches Conference, 9th AIAA Gossamer Spacecraft Forum, 4th AIAA Multidisciplinary Design Optimization Specialists Conference, 2008: 1726. DOI :10.2514/6.2008-1726.
[6] Krovel T. Optimal tuning of PWPF modulator for attitude control (Doctoral dissertation, Master Thesis, Norwegian University of Science and Technology).
[7] Wright JR, Cooper JE. Introduction to aircraft aeroelasticity and loads. John Wiley & Sons; 2008.
[8] Song G, Ma N. Control of shape memory alloy actuators using pulse-width pulse-frequency (PWPF) modulation. Journal of Intelligent Material Systems and Structures. 2003;14(1):15-22. DOI :10.1177/1045389X03014001002.
[9] Zhengshi Y. Simulation of a Position Control System with PWPF Modulator for On-orbit Service (Doctoral dissertation, Technische Universität München).
[10] Wang X, Wang D, Zhu S, Poh EK. Fractional describing function analysis of PWPF modulator. Mathematical Problems in Engineering. 2013. DOI :10.1155/2013/287040.
[11] Horvat K, Kuljaca O, Sijak T. Describing Function Recording with Simulink and MATLAB. In Technology and Engineering Applications of Simulink, 2012.
[12] Song G, Buck NV, Agrawal BN. Spacecraft vibration reduction using pulse-width pulse-frequency modulated input shaper. Journal of guidance, control, and dynamics. 1999;22(3):433-40. DOI :10.2514/2.4415.
[13] Slotine JJ, Li W. Applied nonlinear control. Englewood Cliffs, NJ: Prentice hall; 1991.
[14] Schwartz C, Gran R. Describing function analysis using MATLAB and Simulink. IEEE Control Systems Magazine. 2001;21(4):19-26. DOI :10.1109/37.939940.
[15] Bisplinghoff RL, Ashley H, Halfman RL. Aeroelasticity Addison. Weslwy Co., Mass. 1955.
[16] Hodges DH, Pierce GA. Introduction to structural dynamics and aeroelasticity. cambridge university press; 2011.
[17] Fung YC. An introduction to the theory of aeroelasticity. Courier Dover Publications; 2008.
[18] Fazelzadeh SA, Rasti A, Sadat-Hoseini H. Optimal flutter suppression of nonlinear typical wing section using time-domain finite elements method. Journal of Aerospace Engineering. 2014;27(5):04014028. DOI :10.1061/(ASCE)AS.1943-5525.0000343.
[19] Singh SN, Yim W. State feedback control of an aeroelastic system with structural nonlinearity. Aerospace Science and Technology. 2003;7(1):23-31. DOI :10.1016/S1270-9638(02)00004-4.
[20] Fazelzadeh SA, Mazidi A, Street D. Aeroelastic concepts in civil aircraft wings design. InChallenges in European aerospace, 5th CEAS Air & Space Conference, 2015: 164.
)
