Automated Procedure for Developing Hybrid Computer Simulations of Turbofan Engines. Part 1: General Description PDF Download
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Languages : en
Pages : 128
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Pages : 128
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Author: John R. Szuch
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Languages : en
Pages : 117
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Author: John R. Szuch
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Category : Airplanes
Languages : en
Pages : 132
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Category : Astronautics
Languages : en
Pages : 724
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Category : Aeronautics
Languages : en
Pages : 410
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Category : Aeronautics
Languages : en
Pages : 456
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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
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Category : Government publications
Languages : en
Pages : 1092
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Category : Aeronautics
Languages : en
Pages : 310
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Category : Government publications
Languages : en
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Pages : 38
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Kalman filters are often used to estimate the state variables of a dynamic system. However, in the application of Kalman filters some known signal information is often either ignored or dealt with heuristically. For instance, state variable constraints (which may be based on physical considerations) are often neglected because they do not fit easily into the structure of the Kalman filter. This paper develops two analytic methods of incorporating state variable inequality constraints in the Kalman filter. The first method is a general technique of using hard constraints to enforce inequalities on the state variable estimates. The resultant filter is a combination of a standard Kalman filter and a quadratic programming problem. The second method uses soft constraints to estimate state variables that are known to vary slowly with time. (Soft constraints are constraints that are required to be approximately satis- fied rather than exactly satisfied.) The incorporation of state variable constraints increases the computational effort of the filter but significantly improves its estima- tion accuracy. The improvement is proven theoretically and shown via simulation results. The use of the algorithm is demonstrated on a linearized simulation of a turbofan engine to estimate health parameters. The turbofan engine model con- tains 16 state variables, 12 measurements, and 8 component health parameters. It is shown that the new algorithms provide improved performance in this example over unconstrained Kalman filtering.
