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Multiple Lyapunov Functions with Blending for InducedL2-norm Control of Switched LPV Systems and its Application to an F-16 Aircraft Model

Xu He, Jun Zhao
2012 Asian journal of control  
The proposed method is applied to an F-16 aircraft longitudinal model and the simulation results demonstrate the effectiveness of the approach.  ...  For a switched LPV system where the parameters are grouped into slow-varying and fast-varying parameters, the blending method is used to construct blended Lyapunov functions based on the multiple Lyapunov  ...  An application of the proposed design method to the F-16 aircraft longitudinal model has also been given where the angle of attack and velocity are fast-varying parameters, and time varying altitude is  ... 
doi:10.1002/asjc.607 fatcat:dzifsflzwbh6tfxts5vkwnqlmq

Average Dwell Time Based Smooth Switching Linear Parameter-Varying Proportional-Integral-Derivative Control for an F-16 Aircraft

Bixuan Huang, Bei Lu, Qifu Li, Yanhui Tong
2021 IEEE Access  
The effectiveness of the ADT-based smooth switching control strategy is demonstrated by applying it to the nonlinear longitudinal model of the F-16 aircraft, and the simulation results are compared with  ...  Switching control methods have great potential applications in flight control system design.  ...  ACKNOWLEDGMENT The authors would like to thank anonymous referees and editors for their helpful comments and suggestions.  ... 
doi:10.1109/access.2021.3059900 fatcat:jxgrwpx7qzh4xhlknstbzuamom

A systematic method of smooth switching LPV controllers design for a morphing aircraft

Weilai Jiang, Chaoyang Dong, Qing Wang
2015 Chinese Journal of Aeronautics  
The morphing aircraft is modeled as an LPV system, whose scheduling parameter is the variation rate of the wing sweep angle.  ...  This paper presents a systematic method of smooth switching LPV control for a morphing aircraft with a variable wing sweep angle.  ...  Acknowledgements This study was supported by the National Natural Science Foundation of China (Nos. 61273083 and 61374012).  ... 
doi:10.1016/j.cja.2015.10.005 fatcat:lqgspq6xq5gzvdie2dr7wzbosa

LPV-based Self-adaption Integral Sliding Mode Controller with L2 Gain Performance for a Morphing Aircraft

Qian Wu, Zhenghua Liu, Fanning Liu, Xuekun Chen
2019 IEEE Access  
The method designed in this paper can be extended to general LPV systems. INDEX TERMS Morphing Aircraft, robust control, LPV, integral sliding mode, adaptive control.  ...  Moreover, a parameter-dependent Lyapunov function analysis shows that the designed adaptive integral sliding mode control rate can converge the LPV system trajectories to the integral sliding mode surface  ...  Based on the uncertainty of the morphing aircraft model and the input-output boundary constraints, an adaptive neuron dynamic surface controller is designed by the barrier Lyapunov function.  ... 
doi:10.1109/access.2019.2923313 fatcat:q237we52kvhhjpw5emjt6zexma

Gain Scheduled Control: Switched Polytopic System Approach

Yanze Hou, Qing Wang, Chaoyang Dong
2011 Journal of Guidance Control and Dynamics  
Lu, B., Wu, F., and Kim, S., “Switching LPV Control of an F-16 Aircraft via Controller State Reset,’ JEEE Transactions on Control Systems Technology, Vol. 14, No. 2, 2006, pp. 267-277. doi: 10.1109/TCST  ...  Recent works by Wu and his coworkers propose a switched LPV/linear fractional transformation gain-scheduled method that uses multiple Lyapunov functions instead of acommon Lyapunov function to guarantee  ... 
doi:10.2514/1.51699 fatcat:qm2nwj23bvf6zi4wqmtybmz5em

Stability Analysis of Switched Linear Systems with Locally Overlapped Switching Law

Yanze Hou, Chaoyang Dong, Qing Wang
2010 Journal of Guidance Control and Dynamics  
Lu, B., Wu, F,, and Kim, S., “Switching LPV Control of an F-16 Aircraft via Controller State Reset,” JEEE Transactions on Control Systems Technology, Vol. 14, No. 2, 2006, pp. 267-277. doi: 10.1109/TCST  ...  IV, this method is extended to the combination of common Lyapunov func- tion and average dwell time, and an application to full-envelope flight controller design is illustrated.  ... 
doi:10.2514/1.45795 fatcat:woeaz7opszh3blcpj3txgw6tmm

Robust Model Predictive Control of Shimmy Vibration in Aircraft Landing Gears

M. S. Fallah, S. H. Long, W. F. Xie, Rama Bhat
2008 Journal of Aircraft  
Wada etal. [11] proposed a method for synthesizing the MPC law for linear parameter varying (LPV) systems by using the parameter dependent Lyapunov function (PDLF) and claimed less conservative control  ...  Saeki, M., “Model Predictive Control for Linear Parameter Varying Systems Using Parameter Dependent Lyapunov Function,” 47th [EEE International Midwest Symposium on Circuits and Systems, Vol. 3, Inst.  ... 
doi:10.2514/1.30499 fatcat:ibgxxnqiqranrj7u2zhzqqc22u

Nonlinear Receding Horizon Control of an F-16 Aircraft

Raktim Bhattacharya, Gary J. Balas, M. Alpay Kaya, Andy Packard
2002 Journal of Guidance Control and Dynamics  
The application of receding horizon control (RHC) with the linear, parameter varying (LPV) design methodology to a high-delity, nonlinear F-16 aircraft model is demonstrated.  ...  The highlights are 1) use of RHC to improve upon the performance of a LPV regulator; 2) discussion on details of implementation such as control space formulation, tuning of RHC parameters, computation  ...  The LPV regulator is used to prestabilize the unstable F-16 aircraft and as a control Lyapunov function endpoint penalty in the RHC optimization.  ... 
doi:10.2514/2.4965 fatcat:yv5eqc2mtfddplzevmmfv2qllu

Nonlinear receding horizon control of F-16 aircraft

R. Bhattacharya, G.J. Balas, A. Kaya, A. Packard
2001 Proceedings of the 2001 American Control Conference. (Cat. No.01CH37148)  
The application of receding horizon control (RHC) with the linear, parameter varying (LPV) design methodology to a high-delity, nonlinear F-16 aircraft model is demonstrated.  ...  The highlights are 1) use of RHC to improve upon the performance of a LPV regulator; 2) discussion on details of implementation such as control space formulation, tuning of RHC parameters, computation  ...  The LPV regulator is used to prestabilize the unstable F-16 aircraft and as a control Lyapunov function endpoint penalty in the RHC optimization.  ... 
doi:10.1109/acc.2001.945598 fatcat:3wue5kx5m5dgzoqcbjqsfawhvm

Supervisory fault tolerant control of the GTM UAV using LPV methods

T. Peni, B. Vanek, Z. Szabo, P. Gaspar, J. Bokor
2013 2013 Conference on Control and Fault-Tolerant Systems (SysTol)  
The method is demonstrated on a full six-degrees-of-freedom nonlinear simulation model of the GTM UAV.  ...  Based on the LPV control framework, this is done by introducing fault-specific scheduling parameters.  ...  Irene Gregory and David Cox of the NASA Langley Research Center for making the GTM simulation model available for the purpose of this research.  ... 
doi:10.1109/systol.2013.6693938 fatcat:2bpwawgmrbb2hl2p3gxsoojhei

Supervisory Fault Tolerant Control of the GTM UAV Using LPV Methods

Tamás Péni, Bálint Vanek, Zoltán Szabó, József Bokor
2015 International Journal of Applied Mathematics and Computer Science  
The method is demonstrated on a full six-degrees-of-freedom nonlinear simulation model of the GTM UAV.  ...  Based on the LPV control framework, this is done by introducing fault-specific scheduling parameters.  ...  Irene Gregory and David Cox of the NASA Langley Research Center for making the GTM simulation model available for the purpose of this research.  ... 
doi:10.1515/amcs-2015-0009 fatcat:qgbi2pgkqfcyzkxm2ksxcnehv4

Survey of gain-scheduling analysis and design

D. J. Leith, W. E. Leithead
2000 International Journal of Control  
Thirdly, attention is restricted to continuous scheduling methods and no attempt is made to review the very extensive literature on hybrid/switched systems.  ...  of an appropriate family of linear time-invariant controllers.  ...  This possibility arises from the difficulty of choosing a sufficiently general class of Lyapunov function and is, of course, common to almost all constructive Lyapunov methods.  ... 
doi:10.1080/002071700411304 fatcat:oxv67zumpjecliasoaewuoeivm

Flight evaluation of a sliding mode online control allocation scheme for fault tolerant control

Lejun Chen, Christopher Edwards, Halim Alwi, Masayuki Sato
2020 Automatica  
This paper develops a sliding mode fault tolerant control scheme based on a Linear Parameter Varying (LPV) system representation of the plant.  ...  The scheme includes a control allocation component, which is capable of utilizing the available healthy actuators in the face of actuator faults/failures, in an effort to retain close to nominal fault  ...  Uetake from Nakanihon Air Service for their support in terms of the implementation and evaluations of the sliding mode control scheme on the MuPAL-α.  ... 
doi:10.1016/j.automatica.2020.108829 fatcat:izjqzfrxkrcmvbsepptsyvj4ku

GPMC 2020 Proceedings

2020 2020 2nd IEEE International Conference on Gridding and Polytope Based Modelling and Control (GPMC)  
Gain scheduled lateral and longitudinal baseline controllers are synthesized using the grid-based LPV model of the aircraft. M.  ...  Therefore, the distributed propulsion can be used to control the roll, pitch and yaw motion of the morphing wing aircraft.  ...  ACKNOWLEDGMENT The research presented in this paper was carried out as part of the "Dynamics and Control of Autonomous Vehicles meeting the Synergy Demands of Automated Transport Systems (EFOP-3.6.2-16  ... 
doi:10.1109/gpmc50267.2020.9333817 fatcat:dqn3zean25g3zhwlpgxkysv33q

A Review of Convex Approaches for Control, Observation and Safety of Linear Parameter Varying and Takagi-Sugeno Systems

Francisco-Ronay López-Estrada, Damiano Rotondo, Guillermo Valencia-Palomo
2019 Processes  
These paradigms are capable of hiding the nonlinearities by means of an equivalent description which uses a set of linear models interpolated by appropriately defined weighing functions.  ...  This paper provides a review about the concept of convex systems based on Takagi-Sugeno, linear parameter varying (LPV) and quasi-LPV modeling.  ...  Similarly, an LPV control for switched systems with slow-varying parameters was proposed for an F-16 aircraft model in Ref. [53] by adopting the blending method developed by Ref.  ... 
doi:10.3390/pr7110814 fatcat:3akl5v5yh5bgpeqs5ndp3blvve
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