Regret Analysis of Shrinking Horizon Model Predictive Control

Abstract This paper analyzes the suboptimal implementation of shrinking horizon model predictive control (SHMPC) when a fixed number of solver iterations and a warm-start are utilized at each time-step to solve the underlying optimal control problem (OCP). We derive bounds on the loss of performance (regret) and on the difference between suboptimal SHMPC and optimal solutions. This analysis provides insights and practical guidelines for the implementation of SHMPC under computational limitations. A numerical example of axisymmetric spacecraft spin stabilization is reported. The suboptimal implementation of SHMPC is shown to be capable of steering the system from an initial state into a known terminal set while satisfying control constraints.

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Publication Details

Journal
Journal of Dynamic Systems Measurement and Control
Published
2024-08-23
DOI
https://doi.org/10.1115/1.4066317
Citations
1
Primary Topic
Advanced Control Systems Optimization
Type
article
Field-Weighted Citation Impact
0.33
Controls
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article

Regret Analysis of Shrinking Horizon Model Predictive Control

Miguel Castroviejo-Fernandez, Michele Ambrosino, Jordan Leung, Ilya Kolmanovsky
1 citations
Journal of Dynamic Systems Measurement and Control
Advanced Control Systems Optimization
0.33
article

Regret Analysis of Shrinking Horizon Model Predictive Control

Miguel Castroviejo-Fernandez, Michele Ambrosino, Jordan Leung, Ilya Kolmanovsky
article en
1 citations

Abstract

Abstract This paper analyzes the suboptimal implementation of shrinking horizon model predictive control (SHMPC) when a fixed number of solver iterations and a warm-start are utilized at each time-step to solve the underlying optimal control problem (OCP). We derive bounds on the loss of performance (regret) and on the difference between suboptimal SHMPC and optimal solutions. This analysis provides insights and practical guidelines for the implementation of SHMPC under computational limitations. A numerical example of axisymmetric spacecraft spin stabilization is reported. The suboptimal implementation of SHMPC is shown to be capable of steering the system from an initial state into a known terminal set while satisfying control constraints.

Journal of Dynamic Systems Measurement and ControlVol. 147(2)
University of Michigan (US)
Affordable and clean energy
Openalex Percentile: Top 43%
Advanced Control Systems Optimization
0.33
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