Device for measuring the roll rate or roll attitude of a missile

A rate gyro (10) is arranged in a seeker head of a missile and is stimulated to nutate with its natural nutation frequency in inertial space for the purpose of scanning a field of view. The rotational frequency and the nutation frequency of the rate gyro (10) relative to the missile are determined....

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SCHWARZKOPF, GERHART, DULAT, BERND
Format:	Patent
Sprache:	eng
Schlagworte:	AIMING BLASTING GYROSCOPIC INSTRUMENTS HEATING LIGHTING MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS MECHANICAL ENGINEERING NAVIGATION PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS SURVEYING TESTING WEAPON SIGHTS WEAPONS
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