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Interacting Multiple Model Algorithms for Rotorcraft Regime Recognition

机译:交互多模型算法在旋翼机态识别中的应用

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Regime recognition is a critical tool used for condition-based maintenance, fatigue life prediction, and creation of usage spectra for military and commercial rotorcraft. While a variety of regime recognition algorithms are currently in use, many current algorithms suffer from an over-reliance on training data or poor classification accuracy with respect to the stringent guidelines outlined in ADS-79E. This paper introduces a new type of regime recognition algorithm based on a multiple model adaptive estimation scheme, known as an interacting multiple model (IMM) estimator. IMM estimators use a bank of dynamic models to evaluate the likelihood of the system existing in one of various possible dynamic modes. In the regime recognition context, each mode represents the system operating in a given maneuver regime. Compared with other approaches, IMM estimators offer the benefits of probabilistic regime classification and the incorporation of knowledge of the aircraft flight dynamics, which reduces reliance on training data. This paper presents a novel formulation of an IMM estimator for regime recognition wherein mode probabilities from a bank of IMM filters are combined in Bayesian framework to yield maneuver regime probabilities. Example results for the SH-60B show favorable classification performance in preliminary simulation studies using common maneuvers.
机译:体制识别是用于基于状态的维护,疲劳寿命预测以及为军用和商用旋翼飞机创建使用频谱的关键工具。尽管目前使用各种状态识别算法,但相对于ADS-79E中概述的严格指南,许多当前算法都过度依赖训练数据或分类精度较差。本文介绍了一种基于多模型自适应估计方案的新型状态识别算法,称为交互多模型(IMM)估计器。 IMM估计器使用一组动态模型来评估系统以各种可能的动态模式之一存在的可能性。在状态识别上下文中,每种模式都代表系统在给定的操作状态下运行。与其他方法相比,IMM估计器提供了概率状态分类的优势以及飞机飞行动力学知识的结合,从而减少了对训练数据的依赖。本文提出了一种用于状态识别的IMM估计器的新公式,其中,来自IMM滤波器库的模式概率在贝叶斯框架中组合以产生机动状态概率。 SH-60B的示例结果显示,在使用常规演练的初步模拟研究中,分类性能良好。

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