Kompakte Glasfaser-IMU mit 0,005°/h Kreiselstabilität und ±20g Beschleunigungsmessbereich. Ideal für unbemannte Plattformen, Raketen und Flugsysteme. Betrieb bei -40℃ bis 60℃ bei geringem Stromverbrauch.
Small Size TDFG99IMU Fiber Optic Inertial Unit This compact, lightweight fiber optic inertial unit delivers high precision with low power consumption. Featuring eight-point vibration damping, it ensures reliable performance in high-impact and high-vibration environments. Ideal for pure strapdown applications, it meets the demanding requirements of next-generation unmanned platforms, underwater/torpedo systems, and land, airborne, and missile weapon platforms that require
High Accuracy TDF37IMU0 Fiber Optic Inertial Unit Fiber optic inertial units offer significant advantages including compact size, lightweight design, low power consumption, and high precision accuracy. These units are engineered for pure strapdown system design, meeting the demanding requirements of modern unmanned platforms, underwater/torpedo weapons, and various land, airborne, and missile weapon platforms that require small form factor, high-precision inertial measurement
Hochpräzise Glasfaser-IMU mit 0,01°/h Kreiselstabilität und ±20g Reichweite. Kompaktes, robustes Design für raue Umgebungen in Verteidigungs-, Luft- und Raumfahrt- und Marineanwendungen. Geringer Stromverbrauch, zertifizierte Leistung.
High Accuracy TDF72IMU0 Fiber Optic Inertial Unit This advanced fiber optic inertial unit features eight-point vibration reduction, making it ideal for applications with significant impact and vibration. With its compact design, lightweight construction, low power consumption, and high precision, it provides dynamic measurement of carrier angular and linear motion information for various defense and aerospace platforms. Key Features Eight-point vibration reduction system
TDF71IMU0 faseroptische Trägheitseinheit: kompakt (130×130×110 mm), leicht (≤2,2 kg), geringer Stromverbrauch (≤15 W). Hohe Präzision: 0,01°/h Kreiselstabilität, 20μg Beschleunigungsmesserfehler. Betrieb bei -40℃ bis 60℃, ideal für unbemannte Systeme und Raketenplattformen.
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