Missile Autopilot Design via Neural Koopman Embedding

A learning-based missile autopilot design scheme is proposed, leveraging deep neural networks and Koopman operator theory to facilitate the missile control design process. The proposed method trains a neural Koopman embedding, a deep neural network that approximates the state of the embedded bilinear system for nonlinear missile dynamics using trajectory data. This Koopman-embedded bilinear model enables the systematic design of a state-dependent Riccati equation-based controller with local stability guarantees. The proposed method facilitates a full-envelope missile control design without the intricate synthesis of multiple controllers required for gain scheduling. Numerical simulations validate the effectiveness of the approach, demonstrating its tracking performance and robustness in handling nonlinear missile dynamics.

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Publication Details

Journal
Journal of Aerospace Information Systems
Published
2025-09-12
DOI
https://doi.org/10.2514/1.i011660
Primary Topic
Model Reduction and Neural Networks
Type
article
Field-Weighted Citation Impact
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article

Missile Autopilot Design via Neural Koopman Embedding

Youdan Kim, Jinrae Kim, Youngjun Lee
Journal of Aerospace Information Systems
Model Reduction and Neural Networks
article

Missile Autopilot Design via Neural Koopman Embedding

Youdan Kim, Jinrae Kim, Youngjun Lee
article en

Abstract

A learning-based missile autopilot design scheme is proposed, leveraging deep neural networks and Koopman operator theory to facilitate the missile control design process. The proposed method trains a neural Koopman embedding, a deep neural network that approximates the state of the embedded bilinear system for nonlinear missile dynamics using trajectory data. This Koopman-embedded bilinear model enables the systematic design of a state-dependent Riccati equation-based controller with local stability guarantees. The proposed method facilitates a full-envelope missile control design without the intricate synthesis of multiple controllers required for gain scheduling. Numerical simulations validate the effectiveness of the approach, demonstrating its tracking performance and robustness in handling nonlinear missile dynamics.

Journal of Aerospace Information SystemsVol. 22(10)
Seoul National University (KR)
Openalex Percentile: Top 80%
Model Reduction and Neural Networks
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Missile Autopilot Design via Neural Koopman Embedding — Youdan Kim, Jinrae Kim, et al. · Journal of Aerospace Information Systems (2025) | TGRS Research Map | TGRS