Numerical Discretization Methods for the Discounted Linear-Quadratic Control Problem

This study focuses on the numerical discretization methods for the continuous-time discounted linear-quadratic optimal control problem (LQ-OCP) with time delays. By assuming piecewise constant inputs, we formulate the discrete system matrices of the discounted LQ-OCPs into systems of differential equations. Subsequently, we derive the discrete-time equivalent of the discounted LQ-OCP by solving these systems. This paper presents three numerical methods for solving the proposed differential equations systems: the fixed time-step ordinary differential equation (ODE) method, the step-doubling method, and the matrix exponential method. Our numerical experiment demonstrates that all three methods accurately solve the differential equation systems. Interestingly, the step-doubling method emerges as the fastest among them while maintaining the same level of accuracy as the fixed time-step ODE method.

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Publication Details

Published
2025-06-24
DOI
https://doi.org/10.23919/ecc65951.2025.11187233
Primary Topic
Aerospace Engineering and Control Systems
Type
article
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Numerical Discretization Methods for the Discounted Linear-Quadratic Control Problem

Jan Lorenz Svensen, Steen Hørsholt, John Bagterp Jørgensen, Zhanhao Zhang
Aerospace Engineering and Control Systems
article

Numerical Discretization Methods for the Discounted Linear-Quadratic Control Problem

Jan Lorenz Svensen, Steen Hørsholt, John Bagterp Jørgensen, Zhanhao Zhang
article en

Abstract

This study focuses on the numerical discretization methods for the continuous-time discounted linear-quadratic optimal control problem (LQ-OCP) with time delays. By assuming piecewise constant inputs, we formulate the discrete system matrices of the discounted LQ-OCPs into systems of differential equations. Subsequently, we derive the discrete-time equivalent of the discounted LQ-OCP by solving these systems. This paper presents three numerical methods for solving the proposed differential equations systems: the fixed time-step ordinary differential equation (ODE) method, the step-doubling method, and the matrix exponential method. Our numerical experiment demonstrates that all three methods accurately solve the differential equation systems. Interestingly, the step-doubling method emerges as the fastest among them while maintaining the same level of accuracy as the fixed time-step ODE method.

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Aerospace Engineering and Control Systems
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