详情

原文传递 Enhanced Engine Performance During Emergency Operation Using a Model-Based Engine Control Architecture.

题名：	Enhanced Engine Performance During Emergency Operation Using a Model-Based Engine Control Architecture.
作者：	Csank, J. T.; Connolly, J. W.
关键词：	Engine control, Augmentation, High pressure, Surges, Aircraft engines, Performance prediction, Emergencies, Model reference adaptive control, Risk assessment, Independent variables, Thrust augmentation, Dynamic response, Fail-safe systems, Engine failure, Kalman filters, Simulation, State estimation, Optimization, Aircraft safety
摘要：	This paper discusses the design and application of model-based engine control (MBEC) for use during emergency operation of the aircraft. The MBEC methodology is applied to the Commercial Modular Aero-Propulsion System Simulation 40k (CMAPSS40k) and features an optimal tuner Kalman Filter (OTKF) to estimate unmeasured engine parameters, which can then be used for control. During an emergency scenario, normally-conservative engine operating limits may be relaxed to increase the performance of the engine and overall survivability of the aircraft; this comes at the cost of additional risk of an engine failure. The MBEC architecture offers the advantage of estimating key engine parameters that are not directly measureable. Estimating the unknown parameters allows for tighter control over these parameters, and on the level of risk the engine will operate at. This will allow the engine to achieve better performance than possible when operating to more conservative limits on a related, measurable parameter.
总页数：	Csank, J. T.; Connolly, J. W.
报告类型：	科技报告