State Space Representation of the Open-Loop Dynamics of the Space Shuttle Main Engine

Author:

Duyar Ahmet1,Eldem Vasfi1,Merrill Walter C.2,Guo Ten-Huei2

Affiliation:

1. Department of Mechanical Engineering, Florida Atlantic University, Boca Raton, FL 33431

2. National Aeronautics and Space Administration, Lewis Research Center, Cleveland, Ohio 44135

Abstract

A parameter and structure estimation technique for multivariable systems is used to obtain state space representation of open loop dynamics of the space shuttle main engine (SSME). The parametrization being used is both minimal and unique. The simplified linear models may be used for fault detection studies and control system design and development.

Publisher

ASME International

Subject

Computer Science Applications,Mechanical Engineering,Instrumentation,Information Systems,Control and Systems Engineering

Cited by 8 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Predictive Fault Diagnosis System for Intelligent and Robust Health Monitoring;Journal of Aerospace Computing, Information, and Communication;2012-12

2. Predictive Fault Diagnosis System for Intelligent and Robust Health Monitoring;AIAA Infotech@Aerospace 2010;2010-04-20

3. Damage-Mitigating Control of Power Systems for Structural Durability and High Performance;Journal of Engineering for Gas Turbines and Power;1995-04-01

4. A Simplified Dynamic Model of the Space Shuttle Main Engine;Journal of Dynamic Systems, Measurement, and Control;1994-12-01

5. Damage-Mitigating Control of Mechanical Systems: Part II—Formulation of an Optimal Policy and Simulation;Journal of Dynamic Systems, Measurement, and Control;1994-09-01

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