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Link]
Navabi M, Nasiri N. Modeling and simulating the earth's magnetic field utilizing the 10th generation of IGRF and comparison the linear and nonlinear transformation in order to use in satellite attitude control. Journal of Space Science and Technology. 2010;3(4):45-52. [Persian] [
Link]
Navabi M, Hosseini M. Modeling and spacecraft attitude control using reaction wheel with feedback linearization, its performance study subject to power and EULERINT. Modares Mechanical Engineering. 2018;18(1):51-61. [Persian] [
Link]
Sidi MJ. Spacecraft dynamics and control: a practical engineering approach. Cambridge: Cambridge University Press; 1997. [
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DOI:10.1017/CBO9780511815652]
Navabi M, Tavana M, Mirzaei HR. Attitude control of spacecraft by state dependent Riccati equation and power series expansion of Riccati methods. Journal of Space Science and Technology. 2014;7(4):39-49. [Persian] [
Link]
Aydogan A, Hasturk O. Adaptive LQR stabilization control of reaction wheel for satellite systems. Proceedings of the 14th International Conference on Control, Automation. Robotics and Vision (ICARCV); 2016 Nov 13-15; Phuket, Thailand. IEEE; 2017. p. 1-6. [
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DOI:10.1109/ICARCV.2016.7838849]
Alsharif MA, Arslantas YE, Hölzel MS. A comparison between advanced model-free PID and model-based LQI attitude control of a quadcopter using asynchronous android flight data. Proceedings of the 25th Mediterranean Conference on Control and Automation (MED); 2017 July 3-6; Valletta, Malta. IEEE; 2017. p. 1023-1028. [
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DOI:10.1109/MED.2017.7984252]
Zeng Y, Jiang Q, Liu Q, Jing H. PID vs. MRAC control techniques applied to a quadrotor's attitude. Proceedings of the 2nd International Conference on Instrumentation, Measurement, Computer, Communication and Control; 2012 Dec 8-10; Harbin, China. IEEE; 2013. p. 1086-1089. [
Link]
Navabi M, Soleymanpour S. Standard and robust backstepping control of a spacecraft with inertial uncertainty. Modares Mechanical Engineering. 2015;14(16):112-124. [Persian] [
Link]
Navabi M, Soleymanpour S. Command Filtered modular adaptive backstepping attitude control spacecraft in presence of disturbance torque. Modares Mechanical Engineering. 2015;15(7):285-296. [Persian] [
Link]
Chen F, Jiang R, Zhang K, Jiang B, Tao G. Robust backstepping sliding-mode control and observer-based fault estimation for a quadrotor UAV. IEEE Transactions on Industrial Electronics. 2016;63(8):5044-5056. [
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Navabi M, Mirzaei H. Robust optimal adaptive trajectory tracking control of quadrotor helicopter. Latin American Journal of Solids and Structures. 2017;14(6):1040-1063. [
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DOI:10.1590/1679-78253595]
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DOI:10.2514/6.2018-1868]
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DOI:10.1016/j.automatica.2009.02.025]
Navabi M, Hosseini MR. Investigation in to the effect of kinematic of the space craft attitude control using feedback linearization method. Journal of Space Science and Technology. 2018;11(1):59-71. [Persian] [
Link]
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Navabi M, Davoodi A. Modeling of fuel sloshing in a spacecraft and control it by active control method using nonlinear control. Modares Mechanical Engineering. 2019;19(9):2121-2128. [
Link]
Tafazoli S, Khorasani K. Nonlinear control and stability analysis of spacecraft attitude recovery. IEEE Transactions on Aerospace and Electronic Systems. 2006;42(3):825-845. [
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DOI:10.1109/TAES.2006.248187]
