Description
INS-F40A is a Airborne INS system for uav, helicopter, fixed-wing. Pure-inertial position drift is 20m/60s (ref.) 500m/300s (ref.) (CEP). Heading accuracy reaches 1°secL+0.2°/h (RMS). Alignment completes within ≤5min.
Key performance
- Position accuracy: 20m/60s (ref.) 500m/300s (ref.)
- Heading accuracy: 1°secL+0.2°/h
- Alignment time: ≤5min
Specifications
Key Specifications
| Model |
INS-F40A |
| Alignment Time |
≤5min |
Position Accuracy (CEP)
| Pure Inertial |
20m/60s (ref.) 500m/300s (ref.) |
| INS/GNSS Integrated |
Better than GNSS positioning accuracy |
Heading Accuracy (RMS)
| Pure Inertial |
1°secL+0.2°/h |
| INS/GNSS Integrated |
0.5° |
Attitude Accuracy (RMS)
| Pure Inertial |
0.2° |
| INS/GNSS Integrated |
0.1° |
Velocity Accuracy (RMS)
| Pure Inertial |
—— |
| INS/GNSS Integrated |
0.2m/s |
Full specification sheet (PDF)
Complete mechanical, electrical and performance data including dimension drawings for INS-F40A.
Download PDF
Ordering & customisation
Available for OEM supply with your own label, connector and mounting configuration. Each INS-F40A ships with its individual full-temperature calibration report. State quantity, platform and required accuracy in your enquiry and we reply within one business day with lead time and a formal quotation.
Email: sales@seekergimbal.com | WhatsApp / Phone: +86-18657466579
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