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Retrospective Cost Adaptive Control of Generic Transport ModelrnUnder Uncertainty and Failure

机译:不确定性和故障下通用运输模型的追溯成本自适应控制

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This paper presents a case study on the application of retrospective cost adaptive control to the NASA generic transport model under conditions of uncertainty and failure. To apply retrospective cost adaptive control to the generic transport model, a collection of control architectures is defined, where each architecture has a decentralized adaptation structure in the sense that a performance (error) variable is assigned to each control channel for online decentralized adaptation. Sensor signals may be shared among the channels to account for channel coupling. Then, a series of cases that examine the performance of retrospective cost adaptive control under various conditions is considered, including trim finding, startup, unknown time-varying aircraft dynamics (such as icing and mass variation), unknown flight envelope (including the possibility of conflicting commands), known sensing constraints (a failed air data system), known actuation constraints (requiring differential thrust), unknown sensor failure (stuck and biased airspeed measurement), and unknownactuator failure (severe stroke and rate saturation, dead zone, and jam). For each case, a range of scenarios is considered that captures various commands and performance objectives. Disturbance rejection is included in the form of unknown wind shear.
机译:本文提出了在不确定性和故障条件下将回顾性成本自适应控制应用于NASA通用运输模型的案例研究。为了将回顾性成本自适应控制应用于通用传输模型,定义了一组控制体系结构,其中每个体系结构都具有分散的自适应结构,在这种意义上,性能(错误)变量已分配给每个控制通道以进行在线分散式自适应。传感器信号可以在通道之间共享以解决通道耦合问题。然后,考虑了一系列情况,这些情况研究了在各种条件下的追溯成本自适应控制的性能,包括修剪发现,启动,未知的时变飞机动力学(例如结冰和质量变化),未知的飞行包线(包括可能发生的变化)。相互冲突的命令),已知的感应约束(故障的空气数据系统),已知的致动约束(需要差动推力),未知的传感器故障(卡死和有偏差的空速测量)和未知的执行器故障(严重的冲程和速率饱和,死区和卡塞) )。对于每种情况,都考虑了捕获各种命令和性能目标的一系列方案。干扰抑制以未知风切变的形式包括在内。

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