Impulsive Adaptive Dynamic Programming for Spacecraft Pose Tracking Control Based on Fully Actuated System Model

Xiaoxiang Zhang; Rongyu Jin; Yunhai Geng

doi:10.1016/j.ifacol.2025.11.277

Impulsive Adaptive Dynamic Programming for Spacecraft Pose Tracking Control Based on Fully Actuated System Model

Xiaoxiang Zhang^*
, Rongyu Jin
, Yunhai Geng^*

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology
State Key Laboratory of Micro-Spacecraft Rapid Design and Intelligent Cluster
CAS - Beijing Institute of Control Engineering

Research output: Contribution to journal › Conference article › peer-review

Abstract

This paper develops an impulsive control scheme for spacecraft pose tracking using adaptive dynamic programming. A novel second-order fully actuated system model is formulated on SE(3) to capture the coupled attitude-orbit dynamics. The proposed method employs neural networks to approximate optimal control policies between impulsive actions, overcoming computational complexity while ensuring convergence. The effectiveness of the proposed approach is verified through numerical simulations.

Original language	English
Pages (from-to)	958-963
Number of pages	6
Journal	IFAC-PapersOnLine
Volume	59
Issue number	20
DOIs	https://doi.org/10.1016/j.ifacol.2025.11.277
State	Published - 1 Aug 2025
Event	23th IFAC Symposium on Automatic Control in Aerospace, ACA 2025 - Harbin, China Duration: 2 Aug 2025 → 6 Aug 2025

Keywords

Adaptive dynamic programming
Fully actuated system approach
Impulsive control
Lie group SE(3)
Spacecraft control

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10.1016/j.ifacol.2025.11.277

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title = "Impulsive Adaptive Dynamic Programming for Spacecraft Pose Tracking Control Based on Fully Actuated System Model",

abstract = "This paper develops an impulsive control scheme for spacecraft pose tracking using adaptive dynamic programming. A novel second-order fully actuated system model is formulated on SE(3) to capture the coupled attitude-orbit dynamics. The proposed method employs neural networks to approximate optimal control policies between impulsive actions, overcoming computational complexity while ensuring convergence. The effectiveness of the proposed approach is verified through numerical simulations.",

keywords = "Adaptive dynamic programming, Fully actuated system approach, Impulsive control, Lie group SE(3), Spacecraft control",

author = "Xiaoxiang Zhang and Rongyu Jin and Yunhai Geng",

note = "Publisher Copyright: Copyright {\textcopyright} 2025 The Authors.; 23th IFAC Symposium on Automatic Control in Aerospace, ACA 2025 ; Conference date: 02-08-2025 Through 06-08-2025",

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AU - Geng, Yunhai

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N2 - This paper develops an impulsive control scheme for spacecraft pose tracking using adaptive dynamic programming. A novel second-order fully actuated system model is formulated on SE(3) to capture the coupled attitude-orbit dynamics. The proposed method employs neural networks to approximate optimal control policies between impulsive actions, overcoming computational complexity while ensuring convergence. The effectiveness of the proposed approach is verified through numerical simulations.

AB - This paper develops an impulsive control scheme for spacecraft pose tracking using adaptive dynamic programming. A novel second-order fully actuated system model is formulated on SE(3) to capture the coupled attitude-orbit dynamics. The proposed method employs neural networks to approximate optimal control policies between impulsive actions, overcoming computational complexity while ensuring convergence. The effectiveness of the proposed approach is verified through numerical simulations.

KW - Adaptive dynamic programming

KW - Fully actuated system approach

KW - Impulsive control

KW - Lie group SE(3)

KW - Spacecraft control

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T2 - 23th IFAC Symposium on Automatic Control in Aerospace, ACA 2025

Y2 - 2 August 2025 through 6 August 2025

ER -

Impulsive Adaptive Dynamic Programming for Spacecraft Pose Tracking Control Based on Fully Actuated System Model

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Keywords

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