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NASA-TP-1306
Determination of stability and control parameters of a light airplane from flight data using two estimation methods
Year: 1979
Abstract: Two identification methods, the equation error method and the output error method, are used to estimate stability and control parameter values from flight data for a low-wing, single-engine, general aviation airplane. The estimated parameters from both methods are in very good agreement primarily because of sufficient accuracy of measured data. The estimated static parameters also agree with the results from steady flights. The effect of power different input forms are demonstrated. Examination of all results available gives the best values of estimated parameters and specifies their accuracies.
Subject: AERODYNAMIC
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T17:20:43Z | |
| date available | 2017-09-04T17:20:43Z | |
| date copyright | 01/01/1979 | |
| date issued | 1979 | |
| identifier other | ZQYKAEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std/handle/yse/143903 | |
| description abstract | Two identification methods, the equation error method and the output error method, are used to estimate stability and control parameter values from flight data for a low-wing, single-engine, general aviation airplane. The estimated parameters from both methods are in very good agreement primarily because of sufficient accuracy of measured data. The estimated static parameters also agree with the results from steady flights. The effect of power different input forms are demonstrated. Examination of all results available gives the best values of estimated parameters and specifies their accuracies. | |
| language | English | |
| title | NASA-TP-1306 | num |
| title | Determination of stability and control parameters of a light airplane from flight data using two estimation methods | en |
| type | standard | |
| page | 103 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1979 | |
| contenttype | fulltext | |
| subject keywords | AERODYNAMIC | |
| subject keywords | AIRCRAFT | |
| subject keywords | ANALYSIS | |
| subject keywords | CHARACTERISTICS | |
| subject keywords | CONTROL | |
| subject keywords | EQUATIONS | |
| subject keywords | ESTIMATES | |
| subject keywords | FLIGHT | |
| subject keywords | LEAST | |
| subject keywords | LIGHT | |
| subject keywords | LIKELIHOOD | |
| subject keywords | MAXIMUM | |
| subject keywords | METHOD | |
| subject keywords | MONITORING | |
| subject keywords | MOTION | |
| subject keywords | PARAMETERIZATION | |
| subject keywords | REGRESSION | |
| subject keywords | SQUARES | |
| subject keywords | STABILITY | |
| subject keywords | SURFACES |