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KSINS014C Dual-Axis Fiber Optic Rotating Inertial Navigation System
Product Introduction
The KSINS014 is a dual-axis rotating inertial navigation system that uses high-precision fiber optic gyroscopes and quartz flexible accelerometers to suppress navigation error divergence through rotational modulation. It can output position, speed, attitude, angular rate, linear acceleration and other information in real time. . The system has reserved software and hardware interfaces for satellite receivers and air pressure modules to facilitate user selection. It has software and hardware interfaces for astronomical navigation and visual navigation, and can realize multiple switchable navigation modes of inertial/satellite/atmospheric combinations to meet the needs of UAV attitude control and Navigation and positioning requirements.
Feature
● Has long-endurance pure inertial high-precision navigation function
● A variety of switchable navigation modes including inertial/satellite/atmospheric combinations
● Good vibration-shock-heat composite environmental adaptability
● Has in-situ self-calibration maintenance function
● Have complete BIT design
Application
It can be applied to all types of large and medium-sized long-endurance UAVs.
Technical Specifications
Parameter | KSINS014C | |
Performance indicators | Position Accuracy | 1nmile/12h |
Pitch & Roll Accuracy | <0.0013° | |
Heading Accuracy | < 0.008° | |
Speed Accuracy | <0.1m/s | |
Initialization Time | <13min | |
Mechanical/ electrical interface | Steady state power consumption at normal temperature(W) | <36 |
Power supply(V) | 18~32 | |
Output | RS-422,RS-232,CAN | |
Size(mm) | 180×228×247 | |
Weight(Kg) | <12.5 |