طراحی کنترل‌گر مقاوم غیرخطی و پیاده‌سازی آن بر روی شبیه‌ساز زیرسیستم کنترل وضعیت ماهواره

] M.A.P. Jana, L. Schwartz, C.D. Hall, Historical review of air-bearing simulator, Journal of Guidance, Control and Dynamics, Vol.26, pp.513-522, 2003.

[2] A.H. Tavakoli, A. Kalhor and M. Dehghani, Implementation of three axis attitude controllers for evaluation of  a micro gravity satellite simulator, Journal of Space Science, Vol.5, No.2, pp. 59-68, 2012 (in Persian).

[3] K. Surendran, K. Karthikeyan, M. Dineshkumar and K. Latha, Spacecraft attitude control simulator, IEEE, 2011.

[4]  D. Liwei, S. Shenmin and G. Yng, Attitude control of five freedom  air bearing platform based on fractional order sliding mode, third IEEE International Conference on Instrumentation, Measurement, Computer, Communication and Control, 2013.

[5]  W. R. Wilson, L. L. Jones, M. A. Peck, A Multimodule Planar Air Bearing Testbed for CubeSat-Scale Spacecraft, Journal of Dynamic Systems, Measurement, and Control, Vol. 135, No. 4, pp. 1-10, 2013.

[6]  G. Guglieri, F. Maroglio, P. Pellegrino and L. Torre, Design and development of guidance, navigation and control design algorithms for spacecraft rendezvous and docking experimentation, Acta Astronautica, Vol.94, pp.395-408, 2014.

[7]  J. Jung, S.Y. Park, S.W. Kim, Y.H. Eun, Y.K. Chang, Hardware in loop simulations of spacecraft attitude synchronization using the state dependent Riccati equation technique, Advances in Space Research, Vol.51, pp.434-449, 2013.

[8]  P. Gasbari, M. Sabatini, G.B. Palmerini, Ground tests for vision based determination and control of formation flying spacecraft trajectories, Acta Astronautica, Vol.102, pp. 378-391, 2014.

[9] Z. Song n, H. Li, K. Sun, Finite-time control for nonlinear spacecraft attitude based on terminal sliding mode technique, ISA Transactions, Vol. 53, pp.117–124, 2014.

[10] L. Zhao and Y. Jia, Finite-time attitude tracking control for a rigid spacecraft using time-varying terminal sliding mode techniques, International Journal of Control, pp. 1-13, 2014.

 [11] P. M. Tiwari, S. Janardhanan, M. Nabi, Rigid spacecraft attitude control using adaptive integral second order sliding mode, Aerospace Science and Technology, January 8, 2015.

[12] , K.Zare, H.R.koofigar, adaptive second order sliding mode controller for two input-two output uncertain nonlinear systems and application to a 2-DoF Helicopter model, Modares Mechanical Engineering, Vol.15, No.2, pp.189-199, 2015, in persian

[13]         C. Pukdeboon and A. S. I. Zinober, Control Lyapunov Function Optimal Sliding Mode Controllers For Attitude Tracking Of Spacecraft, Journal of the Franklin Institute, vol. 349, pp. 456-475, 3// 2012.

[14] B. Cong, X. Liu, and Z. Chen, Backstepping Based Adaptive Sliding Mode Control For Spacecraft Attitude Maneuvers, Aerospace Science and Technology, vol. 30, pp. 1-7, 10// 2013.

[15]         C. Pukdeboon, A. S. I. Zinober, and M. W. L. Thein, Quasi-Continuous Higher Order Sliding-Mode Controllers for Spacecraft-Attitude-Tracking Maneuvers, Industrial Electronics, IEEE Transactions on, vol. 57, pp. 1436-1444, 2010.

[16]         A. Doria-Cerezo, P. F. Puleston, and C. Kunusch, Control of an active rectifier with an inductive-capacitive-inductive filter using a Twisting based algorithm, in Industrial Electronics Society, IECON 2013 - 39th Annual Conference of the IEEE, pp. 3416-3421, 2013.

[17]         H. M. Becerra, J. B. Hayet, and C. Sagüés, A single visual-servo controller of mobile robots with super-twisting control, Robotics and Autonomous Systems, vol. 62, pp. 1623-1635, 11// 2014.

[18]G. R. Ansarifar and M. Rafiei, Higher order sliding mode controller design for a research nuclear reactor considering the effect of xenon concentration during load following operation, Annals of Nuclear Energy, vol. 75, pp. 728-735, 1// 2015.

[19]         J. Rivera, J. Espinoza-Jurado, and A. Loukianov, Super-Twisting Air/Fuel Ratio Control for Spark Ignition Engines, Advances and Applications in Sliding Mode Control systems. vol. 576, A. T. Azar and Q. Zhu, Eds., ed: Springer International Publishing, pp. 201-226, 2015.

[20] J. Doyle, B. Francis, A. T. boyd, Feedback Control Theory, Macmillan Publishing Co., 1990.

[21] R. Mohsenipour, M. Nasirian, A. Kashinia, M. Fathi, Design of µ-synthesis Controller for attitude control of micro satelite, Journal of Aerospace Science and Technology, Vol. 8, No. 1, pp. 61-72, 2015. (In Persian)

[22] M. Mirshams, H. Taei, M. Ghobadi, H. Haghi,Gh. Sharifi, Using air bearing based paltform and cold gas thruster actator for satelite attitude dynamics simulation, Modares Mechanical Engineering,Vol. 14, No. 12, 2014 (In Persian).

[23]         A. Aghalari, S. A. Kalhor, M. M. Dehghan, S. H. Cheheltani, Manufacturing and Test of an Attitude Dynamics Simulator for Microsatellites Based on CMG, Journal of Aerospace Science and Technology, Vol. 7, No. 3, pp. 51-67, 2013. (In Persian)

 [24]M. J. Sidi, Spacecraft Dynamics And Control A Practical Engineering Approach: Cambridge University Press, 1997.

[25] M. Malekzadeh, A. Naghash and H.A.Talebi, Robust Attitude and Vibration control of a Nonlinear Flexible Spacecraft, Asian Journal of Control, vol.14, no.2,pp.553-563, 2012.

 [26] Y. Shtessel, C. Edwards, L. Fridman, and A. Levant, Sliding Mode Control and Observation: Springer, 2014.

[27] L. Derafa, A. Benallegue, and L. Fridman, Super twisting control algorithm for the attitude tracking of a four rotors UAV, Journal of the Franklin Institute, vol. 349, pp. 685-699, 3// 2012.