Abstract
Aircraft motion in 3D plane is considered to be of three rotations. First one is roll, second one is pitch and the third one is yaw. Pitch of an aircraft cannot be neglected and it is one of the key features to control an aircraft. The pitch of an aircraft is in unstable state space variable, which leads to instability of an aircraft and a control scheme is required to stabilize the aircraft. In this paper, we propose a control strategy which can stabilize the aircraft system. Simulation results using MATLAB are presented to demonstrate the efficiency of proposed control scheme.
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References
Vidyasagar, M.: Non Linear Systems Analysis, 2nd edn. Prentice Hall, Englewood (1993)
Hauser, J., Sastry, S., Meyer, G.: Nonlinear control design for slightly non-minimum phase systems: application to V/STOL aircraft. Automatica. 28(4), 665–679 (1992)
Benvenuti, L., Di Benedetto, M.D., Grizzle, J.W.: Approximate output tracking for nonlinear non-minimum phase systems with an application to flight control. J. Nonlinear Robust Control 4(3), 397–414 (1994)
Devasia, S., Paden, B.: Exact output tracking for nonlinear time-varying systems. In: Proceedings of the 33rd IEEE Conference on Decision & Control Conference, pp. 2346–2355 (1994)
Ozdemir, U., Kavsaoglu, M.S.: Linear and nonlinear simulations of aircraft dynamics using body axis system. Aircr. Eng. Aerosp. Technol. 80(6), 638–648 (2008)
Devika, K.B., Thomas, S.: Controller technique for robust conflict free sequential flight mode control. In: IEEE Conference on Control Applications (CCA) Part of 2014 IEEE Multi-Conference on Systems and Control Antibes, France, pp. 2066–2071 (2014)
Elsadig, M.A., Elbakri, M.A.: Design of autopilot platform using HILS approach. In: IEEE International Conference on Communication, Control, Computing, and Electronics Engineering (ICCCCCEE), Khartoum, Sudan, pp. 1–6 (2017)
Andrievsky, B., Nikolay, K.K., Kuznetsov, V., Kuznetsova, O.A., Leonov, G.A.: Hidden oscillations in the closed-loop aircraft-pilot system and their prevention. IFAC-PapersOnLine 49(14), 30–35 (2016)
Wenqian, T., Zongyuan, L., Xiangju, Q., Yanyang, W., Liguo, S.: Aircraft-pilot system modeling and pilot control behavior research for airdrop task. IFAC-PapersOnLine 49(32), 177–182 (2016)
Efremov, A.V., Tjaglik, M.S., Tiumentzev, U.V., Wenqian, T.: Pilot behavior modeling and its application to manual control tasksVolume. IFAC-PapersOnLine 49(32), 159–164 (2016)
Kedarisetty, S.: Novel two phase algorithm to design three loop autopilot using parameter plane technique and particle swarm optimization. IFAC-PapersOnLine 49(1), 830–835 (2016)
Etkin, B., Reid, L.D.: Dynamcis of Flight: Stability and Control. Wiley, New York (1996)
Hermann, R., Krener, A.J.: Nonlinear controllability and observability. IEEE Trans. Automat. Cont. 22, 728–740 (1977)
Stevens, B., Lewis, F.L.: Aircraft Control and Simulation, 2nd edn. Wiley, Hoboken (2003)
Hun, R., Tiwari, A., Sinha, N.K.: Design and simulation of autopilot control system for stratospheric airship. IFAC-PapersOnLine 49(1), 712–717 (2016)
Deepa, S.N., Sudha, G.: Longitudinal control of aircraft dynamics based on optimization of PID parameters. Thermo Phys. Aeromech. 23(2), 185–194 (2016)
Rajput, V.S, Jatoth, R.K, Dhanuka, P., Bhasker, B.: Hybrid DE-PSO based pitch controller design for aircraft control system. In: IEEE International Conference on Circuits, Controls, Communications and Computing (I4C), Bangalore, India, pp. 1–6 (2016)
Tomlin, C., Lygeros, J., Benvenuti, L., Sastry, S.: Output tracking for a non-minimum phase dynamic CTOL aircraft model. In: Proceedings of the 34th Conference on Decision & Control, pp. 1867–1872 (1995)
Peter, C., Jan, V.: General aviation digital autopilot design based on LQR/LQG control strategy. In: Digital Avionics Systems Conference (DASC), IEEE/AIAA 36th St. Petersburg, FL, USA, pp. 1–9 (2017)
Zhang, B.I., Morton, B.: Robustness analysis of dynamic inversion control laws applied to nonlinear -AFL pitch-AMIS models. Nonlinear Anal. Theory Methods Appl. 32(4), 501–532 (1998)
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Muhammad Ali, S., Ahmed, S. Design of state feedback controller for an auto pilot: to control the stability of aircraft pitch. Int J Interact Des Manuf 13, 365–372 (2019). https://doi.org/10.1007/s12008-018-0497-1
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DOI: https://doi.org/10.1007/s12008-018-0497-1