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Multiple-Model Adaptive Fault-Tolerant Control of a Planetary Lander

机译:行星着陆器的多模型自适应容错控制

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In this paper we present an approach to fault-tolerant control based on multiple models, switching, and tuning andnits implementation to a hardware-in-the-loop simulation of Delta Clipper Experimental dynamics. The Delta ClippernExperimental is characterized by large control input redundancy, which made it an ideal test bed for evaluation ofnadvanced fault-tolerant and adaptive reconfigurable control strategies. The overall failure detection, identification,nand accommodation architecture is an upgraded version of our Fast Online Actuator Reconfiguration Enhancementn(FLARE) system. The FLARE approach is based on representing different possible fault and failure scenarios usingnmultiple observers, such that the case of nominal (no-failure) operation is covered along with the loss-of-effectiveness,nlock-in-place, and hardover failures of the flight control effectors. Based on a suitably chosen performance criterion,nthe FLARE system quickly detects single or multiple failures and reconfigures the controls, thus achieving either thenoriginal desired performance or graceful performance degradation. In the first stage of the project, the FLAREnsystem was tested on a medium-fidelity simulation of Delta Clipper Experimental dynamics, resulting in excellentnperformance over a large range of single and multiple faults and failures. Following that, in collaboration withnBoeing Phantom Works, the FLARE run-time code was installed at their site and tested on a hardware-in-the-loopntest bed consisting of an electromechanical actuator actuating a gimballed engine as a part of a simulation of the DeltanClipper Experimental dynamics.Alarge number of hardware-in-the-loop simulations were run to cover a dense testcasenmatrix, including cases of up to 10 simultaneous control effector failures. In all cases FLARE was able to quicklynand accurately detect the failures and reconfigure the controls, resulting in excellent overall system performance. Innthis paper we describe the Delta Clipper Experimental and its dynamics model, along with the multiple models,nswitching, and tuning based modification of our FLARE system. This is followed by a description of the experimentalntest bed and a discussion of the results obtained through hardware-in-the-loop testing.
机译:在本文中,我们提出了一种基于多种模型的容错控制方法,切换和调整,并将实现实现到Delta Clipper实验动力学的硬件在环仿真中。 Delta ClippernExperimental具有较大的控制输入冗余,使其成为评估高级容错和自适应可重构控制策略的理想测试平台。整体故障检测,识别和适应架构是我们快速在线执行器重配置增强(FLARE)系统的升级版本。 FLARE方法基于使用多个观察者表示不同的可能故障和故障情况,从而涵盖了标称(无故障)操作的情况以及故障的有效性,就地锁定和故障转移故障。飞行控制效应器。基于适当选择的性能标准,FLARE系统可以快速检测单个或多个故障并重新配置控件,从而实现原始的期望性能或性能下降。在项目的第一阶段,对FLAREnsystem在Delta Clipper实验动力学的中等保真度仿真上进行了测试,从而在大范围的单个和多个故障和失败中表现出了出色的性能。然后,与波音公司的Phantom Works合作,将FLARE运行时代码安装在他们的现场,并在硬件在环测试床上进行了测试,该床由一个机电致动器组成,该机电致动器驱动一个球形发动机,作为DeltanClipper仿真的一部分实验动力学:进行了大量的硬件在环仿真以覆盖密集的测试用例矩阵,包括多达10个同时发生的控制执行器故障的情况。在所有情况下,FLARE都能快速准确地检测出故障并重新配置控件,从而获得出色的整体系统性能。在本文中,我们描述了Delta Clipper实验及其动力学模型,以及基于FLARE系统的多种模型,n切换和调整的修改。接下来是对实验床的描述,以及对通过硬件在环测试获得的结果的讨论。

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