TLH-INS370D-26J series Airborne Strapdown Inertial Navigation and Positioning System
Category: Parts & Components
Model: TLH-INS370D-26J
Product parameters: ① Pure Inertial Navigation (CEP): 1.0 nmile/1h ② Integrated navigation (1 σ): 20m ③ Heading accuracy (RMS): 4.5 ' ④ Horizontal stance (RMS): 1.5 ' ⑤ Combined navigation speed (RMS): 0.1m/s ⑥ Gyroscope zero bias stability (1 σ): ≤ 0.03 °/h Product features: ① High performance, high cost-effectiveness, small size, low weight, low power consumption ② Can integrate inertial navigation, satellite navigation (supporting RTK), vehicle information, etc ③ Full temperature point compensation calibration, strong environmental adaptability ④ Customizable serial output protocol ⑤ Equipped with functions such as power on self-test and periodic self-test ⑥ Applied to electro-optical pods, low orbit satellites, various unmanned aerial vehicles, flying robots, etc