Distortion Analysis and Compensation for a Space Contact HIL Simulator with Force Delay and Dead Zone

A space contact hardware-in-the-loop (HIL) simulator is a key facility for ground testing of space contact processes. It must faithfully reproduce the dynamics in space. Force delay is known to induce instability. To suppress velocity drift from noisy force signals, a dead zone is often introduced. In this study, we show that a dead zone is able to not only induce divergence, but also induce convergence. To address this issue, we propose an integrated compensator that combines a hybrid Smith predictor with a dead zone disturbance observer. It jointly addresses delay and dead zone distortions. The proposed method is effective for both divergent and convergent distortions. Verifications and applications validate the approach.

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Publication Details

Journal
Journal of Aerospace Engineering
Published
2026-02-26
DOI
https://doi.org/10.1061/jaeeez.aseng-6727
Primary Topic
Space Satellite Systems and Control
Type
article
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article

Distortion Analysis and Compensation for a Space Contact HIL Simulator with Force Delay and Dead Zone

Chenkun Qi, Xianchao Zhao, Yan Hu, Huayang Li et al.
Journal of Aerospace Engineering
Space Satellite Systems and Control
article

Distortion Analysis and Compensation for a Space Contact HIL Simulator with Force Delay and Dead Zone

Chenkun Qi, Xianchao Zhao, Yan Hu, Huayang Li, Dongjin Li, Feng Gao
article en

Abstract

A space contact hardware-in-the-loop (HIL) simulator is a key facility for ground testing of space contact processes. It must faithfully reproduce the dynamics in space. Force delay is known to induce instability. To suppress velocity drift from noisy force signals, a dead zone is often introduced. In this study, we show that a dead zone is able to not only induce divergence, but also induce convergence. To address this issue, we propose an integrated compensator that combines a hybrid Smith predictor with a dead zone disturbance observer. It jointly addresses delay and dead zone distortions. The proposed method is effective for both divergent and convergent distortions. Verifications and applications validate the approach.

Journal of Aerospace EngineeringVol. 39(3)
Shanghai Jiao Tong University (CN), China Academy of Launch Vehicle Technology (CN)
Openalex Percentile: Top 45%
Space Satellite Systems and Control
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