Performance Analysis of Three Predictors for Mitigating Input and Output Time Delays

This paper presents a novel extended Kalman filter (EKF)-based nonlinear predictor—the extended Kalman predictor (EKP)—and compares its performance with two linear predictors, the Smith predictor (SP) and the Kalman predictor (KP). A motivating application is telerobotic operation using a predictive display that requires knowledge of the robot pose despite time delays at the input and the output. The paper provides the mathematical formulation of the EKP, as well as the two linear predictors, and demonstrates their use for the simulated flight of a small, fixed-wing uncrewed air vehicle. The EKP performs comparably to the KP when the aircraft motion experiences small perturbations from a nominal trajectory, but the EKP outperforms the KP for larger excursions. The SP performs poorly in every case.

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Publication Details

Journal
Journal of Aerospace Information Systems
Published
2025-02-01
DOI
https://doi.org/10.2514/1.i011466
Primary Topic
Network Time Synchronization Technologies
Type
article
Field-Weighted Citation Impact
0.00

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article

Performance Analysis of Three Predictors for Mitigating Input and Output Time Delays

Craig A. Woolsey, Zakia Ahmed, Nazmus Sakib
Journal of Aerospace Information Systems
Network Time Synchronization Technologies
article

Performance Analysis of Three Predictors for Mitigating Input and Output Time Delays

Craig A. Woolsey, Zakia Ahmed, Nazmus Sakib
article en

Abstract

This paper presents a novel extended Kalman filter (EKF)-based nonlinear predictor—the extended Kalman predictor (EKP)—and compares its performance with two linear predictors, the Smith predictor (SP) and the Kalman predictor (KP). A motivating application is telerobotic operation using a predictive display that requires knowledge of the robot pose despite time delays at the input and the output. The paper provides the mathematical formulation of the EKP, as well as the two linear predictors, and demonstrates their use for the simulated flight of a small, fixed-wing uncrewed air vehicle. The EKP performs comparably to the KP when the aircraft motion experiences small perturbations from a nominal trajectory, but the EKP outperforms the KP for larger excursions. The SP performs poorly in every case.

Journal of Aerospace Information SystemsVol. 22(2)
Virginia Tech (US)
Division of Information and Intelligent Systems
Openalex Percentile: Top 98%
Network Time Synchronization Technologies
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