A circuit for determining the derivatives of an aircraft from flight data and which needs relatively few computation elements at the analog computer is discussed. Since quadratic terms are also taken into account in the analysis, the polar can be determined from the ascertained coefficients in the environment of a point. The results of an evaluation of flight data are discussed. (Author)
Determination of the Derivatives of Longitudinal Motion of an Aircraft from Flight Data by a Model with Automatic Parameter Adjustment
1972
35 pages
Report
Keine Angabe
Englisch
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