Modeling and control for the mode transition of a novel tilt-wing UAV
This paper mainly presents a multibody dynamics model and a novel control method for the mode transition of a new-style distributed propulsion tilt-wing UAV. Base on the technology of tensor flight dynamics, a multibody attitude dynamics model formulated in an invariant tensor form is developed for...
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| Published in | Aerospace science and technology Vol. 91; pp. 593 - 606 |
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| Main Authors | , , |
| Format | Journal Article |
| Language | English |
| Published |
Elsevier Masson SAS
01.08.2019
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| Subjects | |
| Online Access | Get full text |
| ISSN | 1270-9638 1626-3219 |
| DOI | 10.1016/j.ast.2019.05.046 |
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| Abstract | This paper mainly presents a multibody dynamics model and a novel control method for the mode transition of a new-style distributed propulsion tilt-wing UAV. Base on the technology of tensor flight dynamics, a multibody attitude dynamics model formulated in an invariant tensor form is developed for the mode transition such that the dynamics induced by the relative movement of the moving parts (wings and rotors) with respect to the fuselage could be formulated explicitly in the model. The control system is decoupled into two parts, namely the position subsystem and the attitude subsystem subject to input perturbation and external aerodynamic disturbances. A novel finite time altitude tracking controller is designed for position subsystem in terms of the existence of the external disturbances and the perturbations acting on the inputs such that the tilt-wing UAV can converge and move along the desired altitude trajectory in a finite time. Besides, a RISE-based attitude tracking controller is developed to control the attitude subsystem, which guaranteeing robustness to the external disturbances. Numerical simulations are carried out to illustrate the performance of the proposed controllers. |
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| AbstractList | This paper mainly presents a multibody dynamics model and a novel control method for the mode transition of a new-style distributed propulsion tilt-wing UAV. Base on the technology of tensor flight dynamics, a multibody attitude dynamics model formulated in an invariant tensor form is developed for the mode transition such that the dynamics induced by the relative movement of the moving parts (wings and rotors) with respect to the fuselage could be formulated explicitly in the model. The control system is decoupled into two parts, namely the position subsystem and the attitude subsystem subject to input perturbation and external aerodynamic disturbances. A novel finite time altitude tracking controller is designed for position subsystem in terms of the existence of the external disturbances and the perturbations acting on the inputs such that the tilt-wing UAV can converge and move along the desired altitude trajectory in a finite time. Besides, a RISE-based attitude tracking controller is developed to control the attitude subsystem, which guaranteeing robustness to the external disturbances. Numerical simulations are carried out to illustrate the performance of the proposed controllers. |
| Author | Lin, Chenghao Zhou, Yaoming Wang, Yongchao |
| Author_xml | – sequence: 1 givenname: Yongchao surname: Wang fullname: Wang, Yongchao – sequence: 2 givenname: Yaoming surname: Zhou fullname: Zhou, Yaoming email: zhouyaoming@buaa.edu.cn – sequence: 3 givenname: Chenghao surname: Lin fullname: Lin, Chenghao |
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| Cites_doi | 10.1016/j.jfranklin.2017.08.024 10.1016/j.ast.2017.05.022 10.1007/s11071-017-3382-8 10.1109/TIE.2015.2414396 10.1109/TIE.2014.2364982 10.1109/TASE.2015.2434393 10.1007/s11071-015-2387-4 10.1016/j.isatra.2017.01.024 10.1137/S0363012997321358 10.1002/acs.2759 10.1016/j.ast.2015.10.012 10.1109/TRO.2014.2305791 10.1016/j.ast.2017.09.008 10.1109/9.317122 10.1109/TIE.2016.2632682 10.1016/j.jfranklin.2011.06.031 10.1016/j.ast.2017.12.029 10.1016/j.automatica.2013.04.040 10.1016/j.mechatronics.2012.03.003 10.1016/j.automatica.2003.12.007 10.1016/j.sysconle.2008.09.004 10.1109/TAC.2013.2246900 10.1109/TAC.2011.2179869 10.1016/j.isatra.2014.03.010 10.1016/j.ast.2018.08.021 10.1016/j.ast.2018.07.032 10.1016/j.paerosci.2017.03.001 10.1016/j.jfranklin.2016.04.003 10.1109/TAC.2004.831148 10.1007/s00498-005-0151-x 10.1109/TIE.2016.2612618 10.1016/j.automatica.2004.11.029 |
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| Keywords | Attitude tracking Tilt-wing UAV Multibody dynamics model Mode transition Finite time altitude tracking |
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| References | Ghommam, Luque-vega, Castillo-toledo, Saad (br0240) 2016; 353 Bhat, Bernstein (br0150) 2003; 38 Defoort, Floquet, Kokosy, Perruquetti (br0360) 2009; 58 Wang, Cai (br0070) 2015; 47 Jia, Yu, Mei, Chen, Shen, Ai (br0130) 2017; 68 Rothhaar, Murphy, Bacon, Gregory, Grauer, Busan, Croom (br0350) 2014 Li, Zhang, Liu, Zuo, Liu (br0020) 2018; 81 Yao, Deng, Jiao (br0250) 2017; 14 Bhat, Bernstein (br0330) 2005; 17 Cetinsoy, Dikyar, Hancer, Oner, Sirimoglu, Unel, Aksit (br0050) 2012; 22 Zuo, Mallikarjunan (br0090) 2017; 64 Besnard, Shtessel, Landrum (br0120) 2012; 349 Khalil (br0370) 2002 Zheng, Xiong, Luo (br0110) 2014; 53 Deng, Yao (br0260) 2017; 67 br0340 Fang, Wu, Shang, Dong (br0140) 2016; 83 Xian, Dawson, De Queiroz, Chen (br0210) 2004; 49 Xian, De Queiroz, Dawson, McIntyre (br0200) 2004; 40 Meng, Lin, Ren (br0230) 2013; 49 Yildiz, Unel, Demirel (br0060) 2017; 31 Fischer, Hughes, Walters, Schwartz, Dixon (br0270) 2014; 30 Li, Liu, Zhu, Gao, Kaynak (br0280) 2015; 62 Ríos, González-Sierra, Dzul (br0170) 2017; 354 Zhao, Xian, Zhang, Zhang (br0080) 2015; 62 Levant (br0160) 2005; 41 Zipfel (br0310) 2007 Liu, Kreimeier, Stumpf, Zhou, Liu (br0010) 2017; 91 Shao, Meng, Liu, Wang (br0220) 2018; 74 Shevitz, Paden (br0290) 1994; 39 Fischer, Kamalapurkar, Dixon (br0300) 2013; 58 Zhu, Du, Cheng, Chu (br0180) 2017; 88 Polyakov (br0320) 2012; 57 Tyan, Van Nguyen, Kim, Lee (br0030) 2017; 71 Muraoka, Okada, Kubo (br0040) 2009 Huang, Zhu, Zheng, Feroskhan (br0190) 2019; 84 Liu, Zhao, Zuo, Zhong (br0100) 2017; 64 Ríos (10.1016/j.ast.2019.05.046_br0170) 2017; 354 Yildiz (10.1016/j.ast.2019.05.046_br0060) 2017; 31 Wang (10.1016/j.ast.2019.05.046_br0070) 2015; 47 Xian (10.1016/j.ast.2019.05.046_br0210) 2004; 49 Ghommam (10.1016/j.ast.2019.05.046_br0240) 2016; 353 Khalil (10.1016/j.ast.2019.05.046_br0370) 2002 Polyakov (10.1016/j.ast.2019.05.046_br0320) 2012; 57 Defoort (10.1016/j.ast.2019.05.046_br0360) 2009; 58 Xian (10.1016/j.ast.2019.05.046_br0200) 2004; 40 Liu (10.1016/j.ast.2019.05.046_br0010) 2017; 91 Zheng (10.1016/j.ast.2019.05.046_br0110) 2014; 53 Zipfel (10.1016/j.ast.2019.05.046_br0310) 2007 Fang (10.1016/j.ast.2019.05.046_br0140) 2016; 83 Meng (10.1016/j.ast.2019.05.046_br0230) 2013; 49 Li (10.1016/j.ast.2019.05.046_br0020) 2018; 81 Shevitz (10.1016/j.ast.2019.05.046_br0290) 1994; 39 Zhu (10.1016/j.ast.2019.05.046_br0180) 2017; 88 Yao (10.1016/j.ast.2019.05.046_br0250) 2017; 14 Tyan (10.1016/j.ast.2019.05.046_br0030) 2017; 71 Li (10.1016/j.ast.2019.05.046_br0280) 2015; 62 Fischer (10.1016/j.ast.2019.05.046_br0300) 2013; 58 Bhat (10.1016/j.ast.2019.05.046_br0150) 2003; 38 Muraoka (10.1016/j.ast.2019.05.046_br0040) 2009 Jia (10.1016/j.ast.2019.05.046_br0130) 2017; 68 Zhao (10.1016/j.ast.2019.05.046_br0080) 2015; 62 Liu (10.1016/j.ast.2019.05.046_br0100) 2017; 64 Huang (10.1016/j.ast.2019.05.046_br0190) 2019; 84 Besnard (10.1016/j.ast.2019.05.046_br0120) 2012; 349 Shao (10.1016/j.ast.2019.05.046_br0220) 2018; 74 Deng (10.1016/j.ast.2019.05.046_br0260) 2017; 67 Levant (10.1016/j.ast.2019.05.046_br0160) 2005; 41 Fischer (10.1016/j.ast.2019.05.046_br0270) 2014; 30 Bhat (10.1016/j.ast.2019.05.046_br0330) 2005; 17 Rothhaar (10.1016/j.ast.2019.05.046_br0350) 2014 Zuo (10.1016/j.ast.2019.05.046_br0090) 2017; 64 Cetinsoy (10.1016/j.ast.2019.05.046_br0050) 2012; 22 |
| References_xml | – volume: 30 start-page: 845 year: 2014 end-page: 852 ident: br0270 article-title: Nonlinear RISE-based control of an autonomous underwater vehicle publication-title: IEEE Trans. Robot. – volume: 40 start-page: 695 year: 2004 end-page: 700 ident: br0200 article-title: A discontinuous output feedback controller and velocity observer for nonlinear mechanical systems publication-title: Automatica – volume: 22 start-page: 723 year: 2012 end-page: 745 ident: br0050 article-title: Design and construction of a novel quad tilt-wing UAV publication-title: Mechatronics. – year: 2007 ident: br0310 article-title: Modeling and Simulation of Aerospace Vehicle Dynamics – volume: 49 start-page: 1206 year: 2004 end-page: 1211 ident: br0210 article-title: A continuous asymptotic tracking control strategy for uncertain nonlinear systems publication-title: IEEE Trans. Autom. Control – volume: 68 start-page: 299 year: 2017 end-page: 307 ident: br0130 article-title: Integral backstepping sliding mode control for quadrotor helicopter under external uncertain disturbances publication-title: Aerosp. Sci. Technol. – volume: 83 start-page: 1053 year: 2016 end-page: 1068 ident: br0140 article-title: A novel sliding mode controller for small-scale unmanned helicopters with mismatched disturbance publication-title: Nonlinear Dyn. – volume: 58 start-page: 2333 year: 2013 end-page: 2338 ident: br0300 article-title: LaSalle-Yoshizawa corollaries for nonsmooth systems publication-title: IEEE Trans. Autom. Control – volume: 58 start-page: 102 year: 2009 end-page: 108 ident: br0360 article-title: A novel higher order sliding mode control scheme publication-title: Syst. Control Lett. – volume: 88 start-page: 2359 year: 2017 end-page: 2369 ident: br0180 article-title: Hovering control for quadrotor aircraft based on finite-time control algorithm publication-title: Nonlinear Dyn. – volume: 91 start-page: 53 year: 2017 end-page: 66 ident: br0010 article-title: Overview of recent endeavors on personal aerial vehicles: a focus on the US and Europe led research activities publication-title: Prog. Aerosp. Sci. – volume: 39 start-page: 1910 year: 1994 end-page: 1914 ident: br0290 article-title: Lyapunov stability theory of nonsmooth systems publication-title: IEEE Trans. Autom. Control – volume: 84 start-page: 18 year: 2019 end-page: 30 ident: br0190 article-title: Fixed-time autonomous shipboard landing control of a helicopter with external disturbances publication-title: Aerosp. Sci. Technol. – volume: 62 start-page: 5665 year: 2015 end-page: 5676 ident: br0280 article-title: Nonlinear robust attitude tracking control of a table-mount experimental helicopter using output feedback publication-title: IEEE Trans. Ind. Electron. – volume: 57 start-page: 2106 year: 2012 end-page: 2110 ident: br0320 article-title: Nonlinear feedback design for fixed-time stabilization of linear control systems publication-title: IEEE Trans. Autom. Control – volume: 53 start-page: 1350 year: 2014 end-page: 1356 ident: br0110 article-title: Second order sliding mode control for a quadrotor UAV publication-title: ISA Trans. – year: 2009 ident: br0040 article-title: Quad tilt wing VTOL UAV: aerodynamic characteristics and prototype flight publication-title: AIAA Infotech@aerosp. Conf. – volume: 31 start-page: 1245 year: 2017 end-page: 1264 ident: br0060 article-title: Nonlinear hierarchical control of a quad tilt-wing UAV: an adaptive control approach publication-title: Int. J. Adapt. Control Signal Process. – volume: 49 start-page: 2363 year: 2013 end-page: 2372 ident: br0230 article-title: Automatica Robust cooperative tracking for multiple non-identical second-order publication-title: Automatica – volume: 41 start-page: 823 year: 2005 end-page: 830 ident: br0160 article-title: Homogeneity approach to high-order sliding mode design publication-title: Automatica – volume: 64 start-page: 1303 year: 2017 end-page: 1312 ident: br0100 article-title: Robust control for quadrotors with multiple time-varying uncertainties and delays publication-title: IEEE Trans. Ind. Electron. – volume: 47 start-page: 473 year: 2015 end-page: 492 ident: br0070 article-title: Mathematical modeling and control of a tilt-rotor aircraft publication-title: Aerosp. Sci. Technol. – volume: 38 start-page: 751 year: 2003 end-page: 766 ident: br0150 article-title: Finite-time stability of continuous autonomous systems publication-title: SIAM J. Control Optim. – volume: 81 start-page: 348 year: 2018 end-page: 361 ident: br0020 article-title: Nonlinear robust control of tail-sitter aircrafts in flight mode transitions publication-title: Aerosp. Sci. Technol. – year: 2002 ident: br0370 article-title: Nonlinear Systems – volume: 17 start-page: 101 year: 2005 end-page: 127 ident: br0330 article-title: Geometric homogeneity with applications to finite-time stability publication-title: Math. Control Signals Syst. – ident: br0340 – volume: 354 start-page: 6672 year: 2017 end-page: 6691 ident: br0170 article-title: Robust tracking output-control for a quad-rotor: a continuous sliding-mode approach publication-title: J. Franklin Inst. – volume: 349 start-page: 658 year: 2012 end-page: 684 ident: br0120 article-title: Quadrotor vehicle control via sliding mode controller driven by sliding mode disturbance observer publication-title: Adv. Guid. Control Aerosp. Veh. Using Sliding Mode Control Obs. Tech. – volume: 353 start-page: 2344 year: 2016 end-page: 2372 ident: br0240 article-title: Three-dimensional distributed tracking control for multiple quadrotor helicopters publication-title: J. Franklin Inst. – volume: 71 start-page: 30 year: 2017 end-page: 41 ident: br0030 article-title: Comprehensive preliminary sizing/resizing method for a fixed wing – VTOL electric UAV publication-title: Aerosp. Sci. Technol. – volume: 14 start-page: 1524 year: 2017 end-page: 1531 ident: br0250 article-title: RISE-based adaptive control of hydraulic systems with asymptotic tracking publication-title: IEEE Trans. Autom. Sci. Eng. – volume: 62 start-page: 2891 year: 2015 end-page: 2902 ident: br0080 article-title: Nonlinear robust adaptive tracking control of a quadrotor UAV via immersion and invariance methodology publication-title: IEEE Trans. Ind. Electron. – volume: 74 start-page: 145 year: 2018 end-page: 159 ident: br0220 article-title: RISE and disturbance compensation based trajectory tracking control for a quadrotor UAV without velocity measurements publication-title: Aerosp. Sci. Technol. – volume: 67 start-page: 256 year: 2017 end-page: 265 ident: br0260 article-title: Adaptive integral robust control and application to electromechanical servo systems publication-title: ISA Trans. – start-page: 1 year: 2014 end-page: 14 ident: br0350 article-title: NASA Langley distributed propulsion VTOL TiltWing aircraft testing, modeling, simulation, control, and flight test development publication-title: 14th AIAA Aviat. Technol. Integr. Oper. Conf. – volume: 64 start-page: 2944 year: 2017 end-page: 2954 ident: br0090 article-title: L1 adaptive backstepping for robust trajectory tracking of UAVs publication-title: IEEE Trans. Ind. Electron. – volume: 354 start-page: 6672 year: 2017 ident: 10.1016/j.ast.2019.05.046_br0170 article-title: Robust tracking output-control for a quad-rotor: a continuous sliding-mode approach publication-title: J. Franklin Inst. doi: 10.1016/j.jfranklin.2017.08.024 – volume: 68 start-page: 299 year: 2017 ident: 10.1016/j.ast.2019.05.046_br0130 article-title: Integral backstepping sliding mode control for quadrotor helicopter under external uncertain disturbances publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2017.05.022 – volume: 88 start-page: 2359 year: 2017 ident: 10.1016/j.ast.2019.05.046_br0180 article-title: Hovering control for quadrotor aircraft based on finite-time control algorithm publication-title: Nonlinear Dyn. doi: 10.1007/s11071-017-3382-8 – volume: 62 start-page: 5665 year: 2015 ident: 10.1016/j.ast.2019.05.046_br0280 article-title: Nonlinear robust attitude tracking control of a table-mount experimental helicopter using output feedback publication-title: IEEE Trans. Ind. Electron. doi: 10.1109/TIE.2015.2414396 – volume: 62 start-page: 2891 year: 2015 ident: 10.1016/j.ast.2019.05.046_br0080 article-title: Nonlinear robust adaptive tracking control of a quadrotor UAV via immersion and invariance methodology publication-title: IEEE Trans. Ind. Electron. doi: 10.1109/TIE.2014.2364982 – volume: 14 start-page: 1524 year: 2017 ident: 10.1016/j.ast.2019.05.046_br0250 article-title: RISE-based adaptive control of hydraulic systems with asymptotic tracking publication-title: IEEE Trans. Autom. Sci. Eng. doi: 10.1109/TASE.2015.2434393 – volume: 83 start-page: 1053 year: 2016 ident: 10.1016/j.ast.2019.05.046_br0140 article-title: A novel sliding mode controller for small-scale unmanned helicopters with mismatched disturbance publication-title: Nonlinear Dyn. doi: 10.1007/s11071-015-2387-4 – volume: 67 start-page: 256 year: 2017 ident: 10.1016/j.ast.2019.05.046_br0260 article-title: Adaptive integral robust control and application to electromechanical servo systems publication-title: ISA Trans. doi: 10.1016/j.isatra.2017.01.024 – volume: 38 start-page: 751 year: 2003 ident: 10.1016/j.ast.2019.05.046_br0150 article-title: Finite-time stability of continuous autonomous systems publication-title: SIAM J. Control Optim. doi: 10.1137/S0363012997321358 – volume: 31 start-page: 1245 year: 2017 ident: 10.1016/j.ast.2019.05.046_br0060 article-title: Nonlinear hierarchical control of a quad tilt-wing UAV: an adaptive control approach publication-title: Int. J. Adapt. Control Signal Process. doi: 10.1002/acs.2759 – volume: 47 start-page: 473 year: 2015 ident: 10.1016/j.ast.2019.05.046_br0070 article-title: Mathematical modeling and control of a tilt-rotor aircraft publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2015.10.012 – volume: 30 start-page: 845 year: 2014 ident: 10.1016/j.ast.2019.05.046_br0270 article-title: Nonlinear RISE-based control of an autonomous underwater vehicle publication-title: IEEE Trans. Robot. doi: 10.1109/TRO.2014.2305791 – volume: 71 start-page: 30 year: 2017 ident: 10.1016/j.ast.2019.05.046_br0030 article-title: Comprehensive preliminary sizing/resizing method for a fixed wing – VTOL electric UAV publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2017.09.008 – year: 2002 ident: 10.1016/j.ast.2019.05.046_br0370 – volume: 39 start-page: 1910 year: 1994 ident: 10.1016/j.ast.2019.05.046_br0290 article-title: Lyapunov stability theory of nonsmooth systems publication-title: IEEE Trans. Autom. Control doi: 10.1109/9.317122 – volume: 64 start-page: 2944 year: 2017 ident: 10.1016/j.ast.2019.05.046_br0090 article-title: L1 adaptive backstepping for robust trajectory tracking of UAVs publication-title: IEEE Trans. Ind. Electron. doi: 10.1109/TIE.2016.2632682 – volume: 349 start-page: 658 year: 2012 ident: 10.1016/j.ast.2019.05.046_br0120 article-title: Quadrotor vehicle control via sliding mode controller driven by sliding mode disturbance observer publication-title: J. Franklin Inst. doi: 10.1016/j.jfranklin.2011.06.031 – volume: 74 start-page: 145 year: 2018 ident: 10.1016/j.ast.2019.05.046_br0220 article-title: RISE and disturbance compensation based trajectory tracking control for a quadrotor UAV without velocity measurements publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2017.12.029 – volume: 49 start-page: 2363 year: 2013 ident: 10.1016/j.ast.2019.05.046_br0230 article-title: Automatica Robust cooperative tracking for multiple non-identical second-order publication-title: Automatica doi: 10.1016/j.automatica.2013.04.040 – volume: 22 start-page: 723 year: 2012 ident: 10.1016/j.ast.2019.05.046_br0050 article-title: Design and construction of a novel quad tilt-wing UAV publication-title: Mechatronics. doi: 10.1016/j.mechatronics.2012.03.003 – volume: 40 start-page: 695 year: 2004 ident: 10.1016/j.ast.2019.05.046_br0200 article-title: A discontinuous output feedback controller and velocity observer for nonlinear mechanical systems publication-title: Automatica doi: 10.1016/j.automatica.2003.12.007 – volume: 58 start-page: 102 year: 2009 ident: 10.1016/j.ast.2019.05.046_br0360 article-title: A novel higher order sliding mode control scheme publication-title: Syst. Control Lett. doi: 10.1016/j.sysconle.2008.09.004 – volume: 58 start-page: 2333 year: 2013 ident: 10.1016/j.ast.2019.05.046_br0300 article-title: LaSalle-Yoshizawa corollaries for nonsmooth systems publication-title: IEEE Trans. Autom. Control doi: 10.1109/TAC.2013.2246900 – volume: 57 start-page: 2106 year: 2012 ident: 10.1016/j.ast.2019.05.046_br0320 article-title: Nonlinear feedback design for fixed-time stabilization of linear control systems publication-title: IEEE Trans. Autom. Control doi: 10.1109/TAC.2011.2179869 – volume: 53 start-page: 1350 year: 2014 ident: 10.1016/j.ast.2019.05.046_br0110 article-title: Second order sliding mode control for a quadrotor UAV publication-title: ISA Trans. doi: 10.1016/j.isatra.2014.03.010 – volume: 81 start-page: 348 year: 2018 ident: 10.1016/j.ast.2019.05.046_br0020 article-title: Nonlinear robust control of tail-sitter aircrafts in flight mode transitions publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2018.08.021 – volume: 84 start-page: 18 year: 2019 ident: 10.1016/j.ast.2019.05.046_br0190 article-title: Fixed-time autonomous shipboard landing control of a helicopter with external disturbances publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2018.07.032 – start-page: 1 year: 2014 ident: 10.1016/j.ast.2019.05.046_br0350 article-title: NASA Langley distributed propulsion VTOL TiltWing aircraft testing, modeling, simulation, control, and flight test development – volume: 91 start-page: 53 year: 2017 ident: 10.1016/j.ast.2019.05.046_br0010 article-title: Overview of recent endeavors on personal aerial vehicles: a focus on the US and Europe led research activities publication-title: Prog. Aerosp. Sci. doi: 10.1016/j.paerosci.2017.03.001 – volume: 353 start-page: 2344 year: 2016 ident: 10.1016/j.ast.2019.05.046_br0240 article-title: Three-dimensional distributed tracking control for multiple quadrotor helicopters publication-title: J. Franklin Inst. doi: 10.1016/j.jfranklin.2016.04.003 – volume: 49 start-page: 1206 year: 2004 ident: 10.1016/j.ast.2019.05.046_br0210 article-title: A continuous asymptotic tracking control strategy for uncertain nonlinear systems publication-title: IEEE Trans. Autom. Control doi: 10.1109/TAC.2004.831148 – volume: 17 start-page: 101 year: 2005 ident: 10.1016/j.ast.2019.05.046_br0330 article-title: Geometric homogeneity with applications to finite-time stability publication-title: Math. Control Signals Syst. doi: 10.1007/s00498-005-0151-x – year: 2009 ident: 10.1016/j.ast.2019.05.046_br0040 article-title: Quad tilt wing VTOL UAV: aerodynamic characteristics and prototype flight – volume: 64 start-page: 1303 year: 2017 ident: 10.1016/j.ast.2019.05.046_br0100 article-title: Robust control for quadrotors with multiple time-varying uncertainties and delays publication-title: IEEE Trans. Ind. Electron. doi: 10.1109/TIE.2016.2612618 – volume: 41 start-page: 823 year: 2005 ident: 10.1016/j.ast.2019.05.046_br0160 article-title: Homogeneity approach to high-order sliding mode design publication-title: Automatica doi: 10.1016/j.automatica.2004.11.029 – year: 2007 ident: 10.1016/j.ast.2019.05.046_br0310 |
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| SubjectTerms | Attitude tracking Finite time altitude tracking Mode transition Multibody dynamics model Tilt-wing UAV |
| Title | Modeling and control for the mode transition of a novel tilt-wing UAV |
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