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Theoretical And Experimental Investigations Of Sensor Location For Optimal Aeroelastic System State Estimation by Liu%2c Kang.
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1NASA Technical Reports Server (NTRS) 19860019800: Theoretical And Experimental Investigations Of Sensor Location For Optimal Aeroelastic System State Estimation
By NASA Technical Reports Server (NTRS)
One of the major concerns in the design of an active control system is obtaining the information needed for effective feedback. This involves the combination of sensing and estimation. A sensor location index is defined as the weighted sum of the mean square estimation errors in which the sensor locations can be regarded as estimator design parameters. The design goal is to choose these locations to minimize the sensor location index. The choice of the number of sensors is a tradeoff between the estimation quality based upon the same performance index and the total costs of installing and maintaining extra sensors. An experimental study for choosing the sensor location was conducted on an aeroelastic system. The system modeling which includes the unsteady aerodynamics model developed by Stephen Rock was improved. Experimental results verify the trend of the theoretical predictions of the sensor location index for different sensor locations at various wind speeds.
“NASA Technical Reports Server (NTRS) 19860019800: Theoretical And Experimental Investigations Of Sensor Location For Optimal Aeroelastic System State Estimation” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19860019800: Theoretical And Experimental Investigations Of Sensor Location For Optimal Aeroelastic System State Estimation
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 19860019800: Theoretical And Experimental Investigations Of Sensor Location For Optimal Aeroelastic System State Estimation” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - ACTIVE CONTROL - AEROELASTICITY - FEEDBACK - MATHEMATICAL MODELS - MEASURING INSTRUMENTS - PARAMETER IDENTIFICATION - WIND TUNNEL TESTS - DYNAMIC RESPONSE - LARGE SPACE STRUCTURES - SOFTWARE ENGINEERING - UNSTEADY AERODYNAMICS - VIBRATION DAMPING - WIND VELOCITY - Liu, G.
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19860019800
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