___

• Howe D. Aircraft Loading and Structural Layout. London, UK: Professional Engineering Publishing, 2004.
• Currey NS. Aircraft Landing Gear Design: Principles and Practices. Washington D.C., USA: American Institute of Aeronautics and Astronautics Inc, 1988.
• Krüger W, Besselınk I, Cowlıng D. Doan DB, Kortüm W and Krabacher W. Aircraft landing gear dynamics. Simulation and Control, Vehicle System Dynamics 1997; 28:119-158.
• Howell WE, McGebee JR, Daugherty RH and Vogler WA. F-106B airplane active control landing gear drop test performance, Proceedings of the Landing Gear Design Loads Conference, 1991 California,USA.
• McGebee JR and Carden HD. Mathematical model of an active control landing gear for load control during impact and roll-out. NASA Technical Note D-8080,1976.
• Li Y, Gao B and Guan W. Fault-tolerant control for semi-autonomous damper. In: 25th Chinese Control and Decision Conference; 2013 Guiyang, China, pp.623 – 628.
• Zapateiro M, Pozo F, Rossell JM, Karimi HR, Luo N. Landing gear suspension control through adaptive backstepping techniques with H_∞ performance. In: 18th IFAC World Congress;2011 Milano, Italy pp.4809-4814.
• Hua-Lin L, Yong C, Qi H, Jian L. Fuzzy PID control for landing gear based on magneto-rheological (MR) damper. In: Int. Conf. on Apperceiving Computing and Intelligence Analysis, 2009 Chengdu; pp.22-25.
• Ghiringhelli LG and Gualdi S Evalution of landing gear semi-active control system for complete aircraft landing, Aerotechnica Missili e Spazio 2004;83:21-31.
• Sateesh B and Maiti DK. Vibration control of an aircraft nose landing gear due to ground-induced excitation, Proceedings of the Institution of Mechanical Engineers 2010;224: 245-258.
• Ross I and Edson R Application of active control landing gear technology to the A-10 aircraft, NASA CR-166104, 1993, USA.
• Yazici H and Sever M Active control of a non-linear landing gear system having oleo pneumatic shock absorber using robust LQR aproach. Shock and Vibration 2016;1-20.
• Li F, Wei G, Qi W and Xinhe X. Modeling and adaptive control of magneto-rheological buffer system for aircraft landing gear. Applied Mathematical Modelling 2015; 39: 2509-2517
• Toloei AR, Zarchi M and Attaran B. Application of active suspension system to reduce aircraft vibration using PID technique and Bees algorithm. Int J Comput Appl 2014; 98: 17–24.
• Yazici H and Sever M. Active control of a non-linear landing gear system having oleo pneumatic shock absorber using robust linear quadratic regulator approach. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 2017, https://doi.org/10.1177/0954410017713773.
• Sivakumar S and Haran AP. Aircraft random vibration analysis using active landing gears. Journal of Low Frequency Noise Vibration and Active Control 2015; 34: 307-322.
• Gu K, Kharitonov V and Chen J. Stability of Time Delay System. Bostan, USA: Birkhauser: Basel, 2003.
• Zhao Y, Sun W and Gao H. Robust control synthesis for seat suspension systems with actuator saturation and time-varying input delay. Journal of Sound and Vibration 2010; 329: 4335–4353.
• Du H and Zhang, N. H_∞ control of active vehicle suspensions with actuator time delay. Journal of Sound and Vibration 2007; 301: 236–252.
• Ghaoui L. E., Qustry F. and Ait Rami M. A Cone complementarity linearization algorithm for static output feedback and related problems. IEEE Transactions on Automatic Control 1997;42:1171-1176.
• Moon Y.S., Park P., Kwon H.W. and Lee Y.S. Delay-Dependent robust stabilization of uncertain state-delayed systems. International Journal of Control 2001;74:1447-1455
• Yazici H., Guclu R., Kucukdemiral I.B.,Parlakci MNA. Robust delay-dependent H control for uncertain structural systems with actuator delay. Journal of Dynamic Systems, Measurement and Control 2012;134:1-15
• Boyd S., Ghaoui L.E., Feron E., Balakrishnan V Linear Matrix Inequalities in System and Control Theory, Society for Industrial and Applied Mathematics, Philadelphia, USA, 1994.
• Löfberg J. Yalmip: A toolbox for modeling and optimzation in MATLAB, Proc. of the CACSD Conference, 2004, Taipei, Taiwan.
• Strum F, Using SeDuMi 1.02 a Matlab for optimization over symmetric cones, Optimization Methods and Software, 1999;11:625-653.