Research on Longitudinal Control Algorithm for Flying Wing UAV Based on LQR Technology

[1]R.M. Wood and X.S. Bauer, “Flying wings/flying fuselages”, AIAA paper 2001-0311, January 2001, pp. 1-7.10.2514/6.2001-311 Search in Google Scholar

[2]W.R. Sear, “Flying Wing airplanes-The XB-35/YB-49 program”, AIAA paper 80-3036 in Evolution of Aircraft Wing Design Sytnposium, pp. 57-59, March 1980.10.2514/6.1980-3036 Search in Google Scholar

[3]S. Esteban, “Static and dynamic analysis of analysis of an unconventional plane flying wing”, AIAA Atmospheric Flight Mechanics Conference and Exhibit, Montreal, Canada. August 2001, pp. 6-9.10.2514/6.2001-4010 Search in Google Scholar

[4]A.R. Weyl, “Tailless Aircraft and Flying Wings A Study of Their Evolution and Their Problems”, Aircraft Engineering, vol. 16, No. 5, pp. 8-13, January 1945.10.1108/eb031207 Search in Google Scholar

[5]G. Yang, J.G. Sun and Q.H. Li, “Augmented LQR Method for Aeroengine Control Systems”, Journal of Aerospace Power, vol. 19, No. 1, pp. 153-158, February 2004. Search in Google Scholar

[6]W.K. Lai, M. F. Rahmat and N.A. Wahab, “Modeling and controller design of pneumatic actuator system with control valve”, International Journal on Smart Sensing and Intelligent Systems, vol. 5, No. 3, pp. 624-644, September 2012.10.21307/ijssis-2017-499 Search in Google Scholar

[7]R. Ghazali, M. Rahmat, Z. Zulfatman et al., “Perfect tracking control with discrete-time lqr for a non-minimum phase electro-hydraulic actuator system”. International Journal on Smart Sensing and Intelligent Systems, vol. 4, No. 3, pp.424-439, September 2011.10.21307/ijssis-2017-448 Search in Google Scholar

[8]L. Gargouri, A. Zaafouri and A. Kochbati et al., “LQG/ LTR Control of a Direct Current Motor”, Systems, Man and Cybernetics, 2002 IEEE International Conference on. IEEE, vol. 5, pp. 5-10, May 2002. Search in Google Scholar

[9]O. Rehman, B. Fidan and I.R. Petersen, “Minimax LQR control design for a hypersonic flight vehicle”, 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, October 2009.10.2514/6.2009-7291 Search in Google Scholar

[10]R.W. Huang and Y.D Zhao, “Soft landing control of electromagnetic Valve actuation for engines by using LQR”, Tsinghua Science and Technology, vol. 47, No. 8, 2007, pp. 1338-1342. Search in Google Scholar

[11]S.B. McCamish, M. Romano and S. Nolet et al., “Flight testing of multiple-spacecraft control on SPHERES during close-proximity operations”, Journal of Spacecraft and Rockets, vol. 46, No. 6, pp. 1202-1213, November–December 2009. Search in Google Scholar

[12]X.J. Xing, J.G. Yan and D.L. Yuan, “Augmented-stability controller design and its simulation or a UAV based on LQR theory”, Flight Dynamics, vol. 29, No. 5, pp. 54-56, October 2011. Search in Google Scholar

[13]J.W. Choi, G. Daniel and L.R. Mariano, “Control System Modeling and Design for a Mars Flyer, MACH-1 Competition”, AIAA Guidance, Navigation and Control Conference and Exhibit, Honolulu, Hawaii, August 2008. Search in Google Scholar

[14]Y. Tao, “Application of Explicit-Model Following Control technology in the Attitude Control System for the Unmanned Shipboard Helicopter”, Journal of Naval Aeronautical Engineering Institute, vol. 24, No. 5, pp. 543-546. September 2009. Search in Google Scholar

[15]J. Andersson, P. Krus and K. Nilsson, “Optimization as a support for selection and design of aircraft actuation systems”, Proceedings of Seventh AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, St. Louis, USA, September 1998.10.2514/6.1998-4887 Search in Google Scholar

[16]Y.B. Li, W.Z. Liu and Q. Song, “Improved LQG control for unmanned helicopter based on active model in wind environment”, Flight Dynamics, vol. 30, No. 4, pp. 318-322, August 2012. Search in Google Scholar

[17]L. Zhang and Z. Zhou, “Study on Longitudinal Control Laws for High Altitude Long Endurance Tailless Flying-wing Unmanned Aerial Vehicles”, Science Technology and Engineering, vol. 7, No. 16, pp. 1671-1819, August 2007. Search in Google Scholar

[18]M.L. Zhang, “Flight Control System”, National defense of Industry Press, 2nd edn, pp. 4142, 1994. Search in Google Scholar

[19]E.Q. Yang, “Research on the key technology of Unmanned Combat Aerial Vehicle flight control system”, Ph.D. Dissertation, Automation Science and Electrical Engineering Dept. Beijing Univ. of Aeronautics and Astronautics, Beijing, China, May 2006. Search in Google Scholar

[20]G. Garcia, J. Daafouz and J. Bernussou, “Output Feedback Disk Pole Assignment for Systems with Positive Real Uncertainty”, Automatic Control, IEEE Transactions on, vol. 41, No. 9, 1996, pp. 1385-1391.10.1109/9.536516 Search in Google Scholar

[21]D.E. Miller and M. Rossi, “Simultaneous Stabilization With Near Optimal LQR Performance”, Automatic Control, IEEE Transactions on, vol. 46, No. 10, 2001, pp. 1543-1555.10.1109/9.956050 Search in Google Scholar

[22]D.D. Moerder and A. Calise, “Convergence of a Numerical Algorithm for Calculating Optimal Output Feedback Gains”, Automatic Control, IEEE Transactions on, vol. 30, No. 9, 1985, pp. 900-903.10.1109/TAC.1985.1104073Search in Google Scholar