Splitting of flight dynamics equations by using statistical rating
DOI:
https://doi.org/10.18372/2306-1472.2.8962Abstract
Given is the division of linearized fourth-measured system of equations describing aircraft longitudinal motion in two subsystems. This new model contains less parameters to be identified. There are several different transformations necessary to solve division problem named above. It is shown that the application of statistical analysis of residual variances of parameter estimations permits to select most suitable transformationReferences
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Бюшгенс Г. С., Студнев Р.В. Аэродинамика самолета: динамика продольного и бокового движения. - М.: Машиностроение, 1979. - 352 с.
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Касьянов, В. А., & Ефремов, С. Г. (1999). Splitting of flight dynamics equations by using statistical rating. Proceedings of National Aviation University, 2(1), 20–26. https://doi.org/10.18372/2306-1472.2.8962
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AEROSPACE SYSTEMS FOR MONITORING AND CONTROL