[1] HaiYang Chao, YongCan Cao, and YangQuan Chen, Autopilots for Small Unmanned Aerial Vehicles: A Survey, International Journal of Control, Automation, and Systems, 2010.
[2] Abbasi A., Ubaid M. Al-Saggaf, Khalid Munawar, Design of Unmanned Aerial Vehicle Autopilot based on Freescale Qorivva 32-bit Microcontroller, Life Science Journal, 2014.
[3] Duarte Lopes Figueiredo, Autopilot and Ground Control Station for UAV, Thesis to obtain the Master of Science Degree in Aerospace Engineering, Supervisor: Chairperson: Professor João Manuel Lage de Miranda Professor André Calado Marta, Lemos, Member of the Committee: Professor Agostinho Rui Alves da Fonseca, November 2014.
[4] Jose Enrique Ortiz, Development of a Low Cost Autopilot System for Unmanned Aerial Vehicles, Virginia Commonwealth University, Richmond, Virginia, August, 2010.
[5] Hans-Petter Halvorsen, M.Sc., Introduction to Hardware-in-the-Loop Simulation, Telemark University College, Faculty of Technology,Department of Electrical Engineering, Information Technology and Cybernetics.
[6] Christian Köhler, Enhancing Embedded Systems Simulation, 1st Edition, Teubner Verlag Springer Fachmedien Wiesbaden GmbH, 2011.
[7] Kargin V., Design of an Autonomous Landing Control Algorithm for a Fixed Wing UAV, a thesis submitted to the graduate school of natutal and applied sciences of middle east technical university, October 2007.
[8] Garza F.R., Morelli E. A., A collection of Nonlinear Aircraft Simulations in MATLAB, NASA/TM-2003-212145.
[9] Roskam J., Airplane Flight Dynamics and Automatic Flight Controls.The University of Kansas Press, 2001.
[10] Nelson R. C., Flight Stability and Automatic Control, McGraw-Hill, 1998.
[11] Stevens B. and Lewis F..Aircraft Control and Simulation, Second Edition.Wiley, New York, NY, 2003.
[12] Blakelock J. H., Automatic Control of Aircraft and missiles, Second Edition, 1991.
[13] Sadati, S.H., Sabzehparvar, and M., Menhaj, M.B. Nonlinear Adaptive Flight Control Using Dynamic Inversion and Neural Networks Controller, Amirkabir Journal of Science & Research Mechanical Engineering, Vol. 18, No.66, Spring & Summer 2006(In Persian)
[14] D. Enns, Robustness of Dynamic Inversion vs. –synthesis: Lateral-Directional Flight Control Example, Proc. 1990 AIAA Guidance, Navigation, Contr. Conf., August 1990.
[15] Huang C.. et al., Analysis and Simulation of a Nonlinear Control Strategy for High Angle of Attack Maneuvers, Proc. 1990 AIAA Guidance, Navigation, Control Conf., Portland, OR, August 1990.
[16] Zhang, Z., Hu, F. and Li, J. Autonomous flight control system designed for small-scale helicopter based on approximate dynamic inversion, Int. Conf. on Adv. Comp. Cont., 2011, pp. 185–191.
[17] Wang, Q. and Stengel, R. F. A dynamic inversion controller design for miniature Unmanned Aerial Vehicles, Consumer Elec., Comm. & Networks, pp. 1916–1921, 2011.
[18] MacKunis, W., Patre, P. M., Kaizer, M. K., and Dixon, W. E. Asymptotic Tracking for Aircraft via Robust and Adaptive Dynamic Inversion Methods, IEEE Tr. Cont. Sys. Tech., vol. 18, no. 6, pp. 1448–1456, 2010.
[19] Peng Lu, Erik-Jan van Kampen, Cornelis de Visser, Qiping Chu., Aircraft fault-tolerant trajectory control using Incremental Nonlinear Dynamic Inversion, Control Engineering Practice, 57, 2016, pp.126-141.
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