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Forces and moments influencing on uncontrollable aircrafts are considered in this book: calculation methods of powered and passive trajectories; influence of an uncontrollable aircraft oscillation on trajectory of center of mass; influence of launch conditions changes on trajectory of aircrafts flight; basics of methodology of flight table compilation. The system of differential equations of three-dimensional motion, offered in this paper, allows calculating the correction factors of flight table of aircrafts with different methods of stabilization. The calculation methodology of aircrafts dispersion characteristics stabilized during the flight as well as by rotation and finned is considered in this book.