MISSILE CONTROL SYSTEM

The invention relates to the field of military technology, and more particularly to a system for controlling a missile using aerodynamic fins, and can be used in the development of guided missiles, interceptor missiles and ballistic missiles. The technical result is greater missile guidance accuracy...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: YAKOVLEV, Aleksandr Sergeevich, DORONIN, Viktor Valentinovich, SAMONOV, Viktor Alekseevich, SOKOLOVSKIJ, Viktor Vladimirovich, SVETLOV, Vladimir Grigorevich, FILIPPOV, Vladimir Sergeevich, KIRILLOV, Ivan Petrovich
Format: Patent
Sprache:eng ; fre ; rus
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