Event-triggered lifted robust MPC stabilization control for space telescope on dual-rate actuated rigid spacecraft systems

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2024-09-04 DOI:10.1016/j.ast.2024.109553
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Abstract

This study addresses the pose stabilization control problem for enhancing a space telescope mounted on a spacecraft system under a dual-rate actuated setup. An input-lifting approach is utilized to manage the dual rates in the control components, specifically the orbital space telescope and its loading platform. To counteract external spatial perturbations and spacecraft system uncertainties, an integrated control scheme is proposed, combining real-time model parameter estimation, active compensation control, and event-triggered lifted robust model predictive control (ET-LRMPC). The event-triggered mechanism in the proposed algorithm minimizes computational resource consumption while maintaining effective spacecraft control. Numerical simulations demonstrate that the proposed control scheme achieves favorable results under persistent external perturbations and model uncertainties. In terms of the overshoot, the algorithm proposed reduces the control effect by up to 87.1% in the spatial displacement of the payload and 98.6% in the Euler attitude angle compared to the conventional control algorithm. For the control of the base, the amount of overshoots with respect to the conventional control in spatial displacement and Euler attitude angle is reduced by 49% and 97.1%.

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双速率致动刚性航天器系统上空间望远镜的事件触发提升鲁棒 MPC 稳定控制
本研究探讨了在双速率驱动设置下,如何增强安装在航天器系统上的太空望远镜的姿态稳定控制问题。利用输入提升方法来管理控制组件中的双速率,特别是轨道空间望远镜及其加载平台。为了抵消外部空间扰动和航天器系统的不确定性,提出了一种综合控制方案,将实时模型参数估计、主动补偿控制和事件触发提升鲁棒模型预测控制(ET-LRMPC)结合在一起。所提算法中的事件触发机制最大限度地减少了计算资源消耗,同时保持了有效的航天器控制。数值仿真表明,在持续的外部扰动和模型不确定性条件下,所提出的控制方案取得了良好的效果。在过冲方面,与传统控制算法相比,所提出的算法在有效载荷空间位移和欧拉姿态角方面分别降低了高达 87.1% 和 98.6% 的控制效果。在底座控制方面,与传统控制相比,空间位移和欧拉姿态角的过冲量分别减少了 49% 和 97.1%。
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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