Comparison of Three Control Structures for Inducing Higher-Order Sliding Modes

For mitigating the chattering effect in the sliding mode control (SMC), many adaption mechanisms have been proposed to reduce the switching gains. However, less attention is paid to the control structure, which influences the resulting uncertainty term and determines the minimum possible gains. This paper compares three control structures for inducing higher-order sliding modes in finite time: nonlinear dynamic inversion (NDI) based SMC, higher-order sliding mode control (HOSMC) with artificially increased relative degree, and the recently proposed incremental nonlinear dynamic inversion (INDI) based SMC. The latter two control structures have reduced model dependency as compared to NDI-SMC. Moreover, their nominal control increments are found to be approximately equivalent if the sampling interval is sufficiently small and if their gains satisfy certain conditions. Under the same circumstances, the norm value of the resulting uncertainty using INDI-SMC is several orders of magnitude smaller than those using other control structures. For maintaining the sliding modes, the minimum possible gains required by HOSMC approximately equal those needed by INDI-SMC divided by the sampling interval. Nevertheless, these two approaches have comparable chattering degrees, which are effectively reduced as compared to NDI-SMC. The analytical results are verified by numerical simulations.

[1]  Peng Lu,et al.  Aircraft Fault-Tolerant Trajectory Control Using Incremental Nonlinear Dynamic Inversion , 2016 .

[2]  Christopher Edwards,et al.  Adaptive dual-layer super-twisting control and observation , 2016, Int. J. Control.

[3]  Christopher Edwards,et al.  Adaptive continuous higher order sliding mode control , 2016, Autom..

[4]  Jan Albert Mulder,et al.  Robust Flight Control Using Incremental Nonlinear Dynamic Inversion and Angular Acceleration Prediction , 2010 .

[5]  E. van Kampen,et al.  Flight testing of incremental backstepping based control laws with angular accelerometer feedback , 2019 .

[6]  Peng Lu,et al.  Incremental Sliding-Mode Fault-Tolerant Flight Control , 2019, Journal of Guidance, Control, and Dynamics.

[7]  Jie Wang,et al.  Continuous high order sliding mode controller design for a flexible air-breathing hypersonic vehicle. , 2014, ISA transactions.

[8]  Gertjan Looye,et al.  Design and Flight Testing of Incremental Nonlinear Dynamic Inversion-based Control Laws for a Passenger Aircraft , 2018 .

[9]  Pedro Simplício,et al.  An acceleration measurements-based approach for helicopter nonlinear flight control using Incremental Nonlinear Dynamic Inversion , 2013 .

[10]  E. van Kampen,et al.  Flexible Aircraft Gust Load Alleviation with Incremental Nonlinear Dynamic Inversion , 2019 .

[11]  A. Levant Sliding order and sliding accuracy in sliding mode control , 1993 .

[12]  Christopher Edwards,et al.  Continuous higher order sliding mode control with adaptation of air breathing hypersonic missile , 2016 .

[13]  Michael Defoort,et al.  A novel higher order sliding mode control scheme , 2009, Syst. Control. Lett..

[14]  Wu-Chung Su,et al.  An Boundary Layer in Sliding Mode for Sampled-Data Systems , 2000 .

[15]  Peng Lu,et al.  Stability Analysis for Incremental Nonlinear Dynamic Inversion Control , 2018 .

[16]  Ümit Özgüner,et al.  A decentralized variable structure control algorithm for robotic manipulators , 1985, IEEE J. Robotics Autom..

[17]  Vadim I. Utkin,et al.  Adaptive sliding mode control with application to super-twist algorithm: Equivalent control method , 2013, Autom..

[18]  Aleksej F. Filippov,et al.  Differential Equations with Discontinuous Righthand Sides , 1988, Mathematics and Its Applications.

[19]  Christopher Edwards,et al.  Continuous higher order sliding mode control based on adaptive disturbance compensation , 2014, 2014 13th International Workshop on Variable Structure Systems (VSS).

[20]  Arie Levant,et al.  Higher-order sliding modes, differentiation and output-feedback control , 2003 .

[21]  P R Smith,et al.  A SIMPLIFIED APPROACH TO NONLINEAR DYNAMIC INVERSION BASED FLIGHT CONTROL , 1998 .

[22]  Dennis S. Bernstein,et al.  Geometric homogeneity with applications to finite-time stability , 2005, Math. Control. Signals Syst..

[23]  Yuri B. Shtessel,et al.  Continuous finite- and fixed-time high-order regulators , 2016, J. Frankl. Inst..

[24]  Xuerui Wang,et al.  High-Speed Flight of Quadrotor Despite Loss of Single Rotor , 2018, IEEE Robotics and Automation Letters.

[25]  Guido C. H. E. de Croon,et al.  Adaptive Incremental Nonlinear Dynamic Inversion for Attitude Control of Micro Air Vehicles , 2016 .