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COMPREHENSIVE MIXED-SENSITIVITY ON-BLADE CONTROL FOR VIBRATION REDUCTION OF THE EC-145 ROTOR

机译:EC-145转子振动减振的综合混合灵敏度控制

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In this work, we further investigate the use of H_∞ control design for On-Blade Control (OBC). Mixed-Sensitivity H_∞ is an advanced control method developed when reliable Linear-Time-Invariant representations exist and is especially suited for multivariable control problems. The method allows the designer to specify robustness and performance demands and existing optimisation algorithms would provide a controller which optimises over such design objectives. Alotaibi and Morales recently applied the methods to an analytical and validated model available for the EC-145 helicopter. Their work showed that the method is successful in reducing significantly all 4/rev hub loads while controlling directly the rotor thrust only. In this work, we extend this approach to control directly the remaining 4/rev components of the rotor hub loads. This comprehensive approach is compared to the simpler case (thrust control only) and we outweigh benefits and disadvantages. A key outcome from this work is that the performance can be improved by pursuing the comprehensive approach, achieving a further 21% vibration reduction in average across the flight envelope. However the comprehensive approach requires further implementation requirements, such as additional sensors and increased computational power, and more controller parameters to tune which can limit its applications. Both schemes provide the benefit of having a single controller operating over the wide flight envelope, ensuring higher reliability in terms of robustness properties without the performance being too compromised.
机译:在这项工作中,我们进一步调查了H_6控制设计对刀片控制(OBC)的使用。混合敏感性H_∞是一种先进的控制方法,在可靠的线性时不变表示存在时,特别适用于多变量控制问题。该方法允许设计人员指定稳健性和性能需求,并且现有的优化算法将提供一个控制器,该控制器优化在这种设计目标上。 Alotaibi和Morales最近将方法应用于EC-145直升机的分析和验证模型。他们的作品表明,该方法成功地减少了所有4 / Rev集线器载荷,同时仅控制转子推力。在这项工作中,我们将这种方法扩展到直接控制转子集线器负载的剩余4 / Rev组件。将这种综合方法与更简单的案例(仅限推力控制)进行比较,我们超过了益处和缺点。这项工作的一个关键结果是通过追求综合方法可以提高性能,在飞行信封上实现进一步的21%的振动减少。然而,综合方法需要进一步的实施要求,例如额外的传感器和增加的计算能力,以及更多的控制器参数来调整,可以限制其应用。这两种方案都提供了在宽飞行信封上运行的单个控制器的益处,确保在鲁棒性属性方面的可靠性,而不会过于妥协。

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