AN ALGORITHM AND CRITERIA FOR COMPRESSOR CHARACTERISTICS REAL-TIME MODELING AND APPROXIMATION

被引:9
作者
ELGAMMAL, AM
机构
[1] Jet Propulsion Laboratory, Faculty of Mechanical Engineering, Belgrade
来源
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME | 1991年 / 113卷 / 01期
关键词
D O I
10.1115/1.2906517
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Numerous problems are encountered in realizing an adequate real time model for an aircraft engine. The purpose of this article is to propose a systematic approach for modeling and approximating the characteristics of an engine or engine component parts, and to apply this approach to the Viper compressor (VC) characteristics. The proposed approach introduces a set of quantitative model-performance measures. Monitoring these measures makes it possible to take care of the multiple objectives of the model simultaneously and individually, and to attach a guarantee level to the model behavior. A set of (66) models are considered, from which the adequate VC model for real time (RT) simulation purposes is determined.
引用
收藏
页码:112 / 118
页数:7
相关论文
共 13 条
[1]  
Astrom K.J., 2011, COMPUTER CONTROLLED
[2]  
CONVERSE GL, 1984, NASA CR174645
[3]  
DEHOFF RI, 1978, ADV THEORY APPLICATI, V14, P260
[4]  
DEHOFF RI, 1981, THEORY APPLICATIONS
[5]  
Eykhoff Pieter, 1974, SYSTEM IDENTIFICATIO
[6]  
GARLAND WJ, 1989, MAR P INT FOR MATH M
[7]  
HORLOCK JH, 1982, AXIAL FLOW COMPRESSO
[8]  
LEIGH JR, 1989, APPLIED DIGITAL CONT
[9]  
Maine R. E., 1985, AGARD FLIGHT TEST TE, V2
[10]  
MARON MJ, 1987, NUMERICAL ANAL PRACT, P201