Development of aircraft flight computer modeling

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Development of aircraft flight computer modeling is considered. After deriving the vector equations of aircraft general motion, its closure by kinematic equations, vector mapping into the bound coordinate system, the matrix differential equation system is obtained.

Adequacy, vector, differential equations, matrix operations, theorems of mechanics, flight modeling, coordinate system

Короткий адрес: https://sciup.org/148201256

IDR: 148201256

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