Place of Origin:
China (Mainland)
ชื่อแบรนด์:
Kacise
ได้รับการรับรอง:
certificate of explosion-proof, CE
Model Number:
KsINS-G110A/B
วิดีโอ
วิดีโอ
KsINS-G110A/B dual-axis fiber optic rotating inertial navigation system
product description:
KsINS-G110A/B 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.
G110A G110B
Features:
● 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 fields and application modes:
It can be applied to all types of large and medium-sized long-endurance UAVs.
Performance indicators :
| Align time | Normal alignment on the ground: ≤ 13min |
| Emergency alignment: ground alignment 30s + air alignment 15min | |
| Position Accuracy (CEP) | Pure inertia: 1nmile/12h |
| Speed Accuracy (RMS) | Pure inertia: 1m/s/12h |
| Heading alignment accuracy (RMS) | ≤ 0.5′ |
| Heading Keeping Accuracy (RMS) | 0.03°(12h) |
| Attitude maintenance accuracy (RMS) | 0.015°(12h) |
Application environment :
| Working/storage temperature(℃) | -55℃ ~+70℃ |
| Dynamic Range | Angular velocity: ±300°/s; Acceleration: -30g ~ +30g |
| Mechanical properties |
Endurance shock environment: half sine wave 20g, 11ms Endurance vibration environment: typical drone vibration environment |
Physical properties:
| Dimensions | 180mm×228mm×247mm | 180mm×268mm×250mm |
| Installation method | Bracket installation | Aviation bracket installation |
| Installation dimensions |
Bracket installation size: 200mm×224mm Flange installation size: 176mm×198mm |
Bracket installation size: 280mm×190mm |
| weight | Host ≤ 12.5kg; bracket ≤ 1.5kg | Host ≤ 12.5kg; bracket ≤ 1.5kg |
External Interface:
| powered by | 18V~36V DC, power consumption ≤ 36W, allowed power interruption is no more than 5ms |
| Input/output interface |
7 channels RS-422, 1 channel RS-232; 2 channels CAN (FD) 1 channel 1M 1553B, 1 channel 4M1553B |
| Data output frequency | 200Hz (typical) |
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