Precision preview-based stable-inversion for nonlinear nonminimum-phase systems: the VTOL example

DOI10.1016/j.automatica.2006.08.007zbMath1140.93391OpenAlexW2048819743MaRDI QIDQ864296

Santosh Devasia, Qingze Zou

Publication date: 13 February 2007

Published in: Automatica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.automatica.2006.08.007

zbMATH Keywords

output trackingstable inversionVTOL aircraftaircraft guidancenonlinear nonminimum-phase systemspreview-based approach

Mathematics Subject Classification ID

Related Items (21)

Inversion-based output tracking and unknown input reconstruction of square discrete-time linear systems ⋮ Nonlinear adaptive tracking control of non-minimum phase hypersonic flight vehicles with unknown input nonlinearity ⋮ Optimal transient performance under output set-point reset ⋮ Precision preview-based stable-inversion for nonlinear nonminimum-phase systems: the VTOL example ⋮ Accurate output tracking for nonminimum phase nonhyperbolic and near nonhyperbolic systems ⋮ Block approach to analysis and design of the invariant nonlinear tracking systems ⋮ Simultaneous hysteresis‐dynamics compensation in high‐speed, large‐range trajectory tracking: A data‐driven iterative control ⋮ Inversion-based optimal output tracking-transition switching with preview for nonminimum-phase linear systems ⋮ Stable inversion of LPTV systems with application in position-dependent and non-equidistantly sampled systems ⋮ A general framework for approximated model stable inversion ⋮ Feedback methods for inverse simulation of dynamic models for engineering systems applications ⋮ The design of smooth switching control with application to V/STOL aircraft dynamics under input and output constraints ⋮ Investigation of inverse simulation for design of feedforward controllers ⋮ Spline Based Pseudo-Inversion of Sampled Data Non-Minimum Phase Systems for an Almost Exact Output Tracking ⋮ Optimal preview control for discrete-time systems in multirate output sampling ⋮ Optimal preview-based stable-inversion for output tracking of nonminimum-phase linear systems ⋮ Trajectory tracking in aircraft landing operations management using the adaptive neural fuzzy inference system ⋮ Inversion-based control of a vehicle with a clutch using a switched causal modelling ⋮ Pre-Actuation and Optimal State Transition Based Precise Tracking for Maximum Phase System ⋮ A mixed numerical–analytical stable pseudo‐inversion method aimed at attaining an almost exact tracking ⋮ The application of parameter sensitivity analysis methods to inverse simulation models

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