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- W2313253319 abstract "In this paper several parameter/state stimation methods for determination of drag polars from flight data are described and evaluated for unstable/augmented aircraft. The model-based and non-model-based approaches are considered. The roller coaster and wind-up-turn maneuver dynamic response data are generated in a flight simulator at various flight conditions and the typical performance results are presented. A novel approach to estimate the drag polar has been considered and evaluated. It is found that the non-model-based approaches perform better than the model-based approaches. Classically the model-based approaches have been used for determination of drag polars. The merits of the non-model-based approach are that it does not require specifying the detailed model of the aerodynamic coefficients and it can be suitably used for on-line estimation of drag polars from the flight data." @default.
- W2313253319 created "2016-06-24" @default.
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- W2313253319 date "2000-01-10" @default.
- W2313253319 modified "2023-09-25" @default.
- W2313253319 title "Evaluation of methods for determination of drag polars of unstable/augmented aircraft" @default.
- W2313253319 cites W2043701952 @default.
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- W2313253319 doi "https://doi.org/10.2514/6.2000-501" @default.
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