Commenced in January 2007
Paper Count: 30578
Robust Control of a Dynamic Model of an F-16 Aircraft with Improved Damping through Linear Matrix Inequalities
Abstract:This work presents an application of Linear Matrix Inequalities (LMI) for the robust control of an F-16 aircraft through an algorithm ensuring the damping factor to the closed loop system. The results show that the zero and gain settings are sufficient to ensure robust performance and stability with respect to various operating points. The technique used is the pole placement, which aims to put the system in closed loop poles in a specific region of the complex plane. Test results using a dynamic model of the F-16 aircraft are presented and discussed.
Digital Object Identifier (DOI): doi.org/10.5281/zenodo.1128927Procedia APA BibTeX Chicago EndNote Harvard JSON MLA RIS XML ISO 690 PDF Downloads 1070
 M. L. Fravolini, T. Yucelen, J. Muse and P. Valigi, ”Analysis and design of adaptive control systems with unmodeled input dynamics via multiobjective convex optimization,” 2015 American Control Conference (ACC), Chicago, IL, 2015, pp. 1579-1584.
 B. Xu, X. Huang, D. Wang and F. Sun, ”Dynamic surface control of constrained hypersonic flight models with parameter estimation and actuator compensation”. Asian Journal of Control, v. 16, n. 1, p. 162-174, 2014.
 ∅. H. Holhjem, L1 Adaptive Control of the Inner Control Loops of an F-16 Aircraft. 2012.
 X. He, J. Zhao and G. M. Dimirovski, ”A blending method control of switched LPV systems with slow-varying parameters and its application to an F-16 aircraft model,” Control Conference (CCC), 2011 30th Chinese, Yantai, 2011, pp. 1765-1770.
 X. He, G. M. Dimirovski and J. Zhao, ”Control of switched LPV systems using common Lyapunov function method and an F-16 aircraft application,” Systems Man and Cybernetics (SMC), 2010 IEEE International Conference on, Istanbul, 2010, pp. 386-392.
 S. Seshagiri and E. Promtun, ”Sliding mode control of F-16 longitudinal dynamics,” 2008 American Control Conference, Seattle, WA, 2008, pp. 1770-1775.
 F. Liao, J. L. Wang and G. Yang, ”Reliable robust flight tracking control: an LMI approach,” in IEEE Transactions on Control Systems Technology, vol. 10, no. 1, pp. 76-89, Jan 2002.
 V. A. F. de Campos, J. J. da Cruz, and L. C. Zanetta. ”Robust and optimal adjustment of power system stabilizers through linear matrix inequalities.” International Journal of Electrical Power & Energy Systems, 2012, pp. 478-486.
 B. L. Stevens, F. L. Lewis, and E. N. Johnson. ”Aircraft Control and Simulation: Dynamics, Controls Design, and Autonomous Systems”. John Wiley & Sons, 2015.
 R. S. Russell, ”Non-linear f-16 simulation using simulink and matlab”. University of Minnesota, Tech. paper, 2003.
 M. Chilali, P. Gahinet and P. Apkarian, ”Robust pole placement in LMI regions,” in IEEE Transactions on Automatic Control, vol. 44, no. 12, pp. 2257-2270, Dec 1999.
 F. Escudero Scavoni, A. S. e Silva, A. Trofino Neto and J. M. Campagnolo, ”Design of robust power system controllers using linear matrix inequalities,” Power Tech Proceedings, 2001 IEEE Porto, Porto, 2001, pp. 6 pp. vol.2-.
 Boyd S., El Ghaoui L., Feron E., Balakrishnan V. Linear matrix inequalities in system and control theory. Philadelphia: SIAM; 1994.