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> Search Results: Stefańska, A.
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Original version of the author's contribution in proceedings, page 918, section DYN.:
PDF
THE USE OF GYROSCOPIC EXECUTIVE SYSTEM FOR HOMING OF THE MISSILE ON THE AERIAL TARGET
Stefański, K.
;
Stefańska, A.
The paper considers the possibility of use of the executive system for missile flight control in the form of fast rotating rotor, versatile suspended in the rocket body. [...]
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