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Abstract: This paper investigates the state-tracking control problem in conversion mode of a tilt-rotor aircraft with a switching modeling method and a smooth interpolation technique. Based on the nonlinear model of the conversion mode, a switched linear model is developed by using the Jacobian linearization method and designing the switching signal based on the mast angle. Furthermore, an H_∞ state-tracking control scheme is designed to deal with the conversion mode control issue. Moreover, instead of limiting the amplitude of control inputs, a smooth interpolation method is developed to create bumpless performance. Finally, the XV-15 tilt-rotor aircraft is chosen as a prototype to illustrate the effectiveness of this developed control method.

基于切换系统建模的倾转旋翼机过渡模式光滑跟踪控制

[1]Abà A, Barra F, Capone P, et al., 2020. Mathematical modelling of gimballed tilt-rotors for real-time flight simulation. Aerospace, 7(9):124.

[2]Allerhand LI, Shaked U, 2011. Robust stability and stabilization of linear switched systems with dwell time. IEEE Trans Autom Contr, 56(2):381-386.

[3]Barra F, Godio S, Guglieri G, et al., 2019. Implementation of a comprehensive mathematical model for tilt-rotor real-time flight simulation. 45^th European Rotorcraft Forum, Article 0020.

[4]Chen C, Zhang JY, Zhang DB, et al., 2017. Control and flight test of a tilt-rotor unmanned aerial vehicle. Int J Adv Robot Syst, 14(1).

[5]Daafouz J, Geromel JC, Deaecto GS, 2012. A simple approach for switched control design with control bumps limitation. Syst Contr Lett, 61(12):1215-1220.

[6]Fei ZY, Chen WZ, Zhao XD, et al., 2023. Stabilization of switched linear neutral systems with time-scheduled feedback control strategy. IEEE Trans Autom Contr, 68(2):1093-1100.

[7]Harendra PB, Joglekar MJ, Gaffey TM, et al., 1973. V/STOL Tilt Rotor Study. Volume 5: a Mathematical Model for Real Time Flight Simulation of the Bell Model 301 Tilt Rotor Research Aircraft. Technical Report No. BELL-301-099-001-VOL-5, Bell Helicopter Co., Fort Worth, TX, USA.

[8]Hou LL, Ma X, Sun HN, 2022. Stabilization of switched linear systems under asynchronous switching subject to admissible edge-dependent average dwell time. Front Inform Technol Electron Eng, 23(5):810-822.

[9]Kleinhesselink KM, 2007. Stability and control modeling of tiltrotor aircraft. MS Thesis, University of Maryland, College Park, MD, USA.

[10]Kong ZW, Lu Q, 2018. Mathematical modeling and modal switching control of a novel tiltrotor UAV. J Robot, 2018:8641731.

[11]Li YL, Wang HQ, Zhao XD, et al., 2022. Event-triggered adaptive tracking control for uncertain fractional-order nonstrict-feedback nonlinear systems via command filtering. Int J Robust Nonl Contr, 32(14):7987-8011.

[12]Li Z, Xia P, 2018. Aeroelastic modelling and stability analysis of tiltrotor aircraft in conversion flight. Aeronaut J, 122(1256):1606-1629.

[13]Maisel MD, Giulianetti DJ, Dugan DC, 2000. The History of the XV-15 Tilt Rotor Research Aircraft from Concept to Flight. NASA, Washington, DC, USA. https://history.nasa.gov/monograph17.pdf

[14]Roy S, Baldi S, Ioannou PA, 2022. An adaptive control framework for underactuated switched Euler–Lagrange systems. IEEE Trans Autom Contr, 67(8):4202-4209.

[15]Rysdyk R, Calise AJ, 2005. Robust nonlinear adaptive flight control for consistent handling qualities. IEEE Trans Contr Syst Technol, 13(6):896-910.

[16]Rysdyk RT, Calise AJ, 1999. Adaptive model inversion flight control for tilt-rotor aircraft. J Guid Contr Dyn, 22(3):402-407.

[17]Shi S, Fei ZY, Zhao XD, 2021. Time-scheduled observer design for switched linear systems with unknown inputs. Sci China Inform Sci, 65(7):179204.

[18]Tang FH, Niu B, Zong GD, et al., 2022. Periodic event-triggered adaptive tracking control design for nonlinear discrete-time systems via reinforcement learning. Neur Netw, 154:43-55.

[19]Thompson TH, 1990. The Bell Helicopter XV-3 and XV-15 experimental aircraft—lessons learned. Aircraft Design, Systems and Operations Conf.

[20]Wang XH, Cai LL, 2015. Mathematical modeling and control of a tilt-rotor aircraft. Aerosp Sci Technol, 47:473-492.

[21]Wang YE, Sun XM, Mazenc F, 2016. Stability of switched nonlinear systems with delay and disturbance. Automatica, 69:78-86.

[22]Xiang WM, 2015. On equivalence of two stability criteria for continuous-time switched systems with dwell time constraint. Automatica, 54:36-40.

[23]Yang D, Zhao J, 2019. H∞ bumpless transfer for switched LPV systems and its application. Int J Contr, 92(8):1945-1958.

[24]Ye J, Roy S, Godjevac M, et al., 2021. A switching control perspective on the offshore construction scenario of heavy-lift vessels. IEEE Trans Contr Syst Technol, 29(1):470-477.

[25]Yuan S, Zhang LX, De Schutter B, et al., 2018. A novel Lyapunov function for a non-weighted L2 gain of asynchronously switched linear systems. Automatica, 87:310-317.

[26]Zhao H, Zong GD, Zhao XD, et al., 2023. Hierarchical sliding-mode surface-based adaptive critic tracking control for nonlinear multiplayer zero-sum games via generalized fuzzy hyperbolic models. IEEE Trans Fuzzy Syst, 31(11):4010-4023.

[27]Zhao XD, Zhang LX, Shi P, et al., 2012. Stability and stabilization of switched linear systems with mode-dependent average dwell time. IEEE Trans Autom Contr, 57(7):1809-1815.

[28]Zhao Y, Zhao J, 2020. H∞ reliable bumpless transfer control for switched systems with state and rate constraints. IEEE Trans Syst Man Cybern Syst, 50(19):3925-3935.

[29]Zhao Y, Zhao J, Fu J, et al., 2020. Rate bumpless transfer control for switched linear systems with stability and its application to aero-engine control design. IEEE Trans Ind Electron, 67(6):4900-4910.