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飞控与探测:2025,8(6):01-10
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基于改进型PILCO方法的变外形飞行器姿态控制
(1.北京航天自动控制研究所;2.宇航智能控制技术全国重点实验室)
Attitude Control for Morphing Aircraft Based on Improved PILCO Method
(1.Beijing Aerospace Automatic Control Institute;2.National Key Laboratory of Science and Technology on Aerospace Intelligence Control)
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中文摘要: 变外形飞行器因其姿态控制面临模型的不确定性而受到关注。基于概率推理学习控制(Probabilistic Inference for Learning Control,PILCO)方法不依赖准确模型,以概率表征不确定性并通过数据驱动优化策略,在系统带有不确定性的控制问题中取得初步进展,但现有研究在处理含高阶伺服模型和复杂工况时仍有局限。基于此,提出了两类改进型PILCO 方法:一是采用基于非马尔可夫过程的历史多拍策略解决了高阶伺服模型带来的控制品质下降问题;二是使用基于多任务学习的多代理模型代价推理和梯度加权的方式提升了控制系统在风干扰下的鲁棒性。以低速变展长验证飞行器为对象,通过数学仿真验证了改进型PILCO 方法独立使用和结合使用时的有效性。
Abstract:Morphing aircraft have attracted attention due to the uncertainties faced in attitude control. Probabilistic Inference for Learning Control (PILCO) methods, which do not rely on accurate models and represent uncertainties probabilistically while optimizing strategies through data-driven approaches, have achieved preliminary progress in the control problems with systematic uncertainties. However, existing studies still face limitations when dealing with high-order servo models and complex operating conditions. This paper proposes two improved PILCO methods that address the degradation of control performance caused by high-order servo models by using a multi-step history policy based on non-Markov processes. Additionally, it enhances the robustness of the control system under wind disturbances through multi-task learning based cost inference of multi-surrogate model and gradient weighting approaches. Using a low-speed morphing wing aircraft as the test object, the effectiveness of the improved PILCO control method was validated through mathematical simulations when used independently and in combination.
文章编号:20250601     中图分类号:TP181; TP273+.4    文献标志码:A
基金项目:国家自然科学基金(U21B2028)
引用文本:
李嘉瑞,柳嘉润,李竞元,钟鸿豪,张远.基于改进型PILCO方法的变外形飞行器姿态控制[J].飞控与探测,2025,8(6):01-10.