Small Aircrafts
Mid-Term Navigation Systems
SKYLINE Mark V 150 INS
Aerial Navigation System
The Skyline Mark V 150 Inertial Navigation System (INS) is a tactical grade aerial navigation system with heading and roll/pitch accuracy in GNSS denied environments. The Skyline Mark V 150 is a GPS-embedded inertial navigation system, capable of combining external sensor data (GPS, magnetic compass, etc.) with a closed loop FOG based IMU via a sophisticated Kalman Filter. Mark V 150 is available either in a standard format or tailor-made to customer requirements.
Compatible for the following applications:
Unmanned Aerial Vehicles
HALE and MALE UAV's
Satcom Antennas
Directional antenna pointing
SKYLINE Mark V 150 Benefits
Maintenance free
No re-calibration required
Cost effective solution.
For air platforms in the GPS-denied battlefield
Open architecture
Flexibility to integrate with customer sensors
ITAR-Free
Our products are ITAR-free and are entirely designed and developed in-house
Technical Information
The Skyline Mark V 150 is a tactical grade air navigation system, containing closed-loop fiber optic gyro technology. It is a versatile inertial navigation system and comes in a variety of configurations.
Skyline Mark V150 INS_V3
| Parameter | Performance | ||
|---|---|---|---|
| OUTPUT | HYBRID MODE RMS VALUES | AHRS MODE RMS VALUES | |
| STANDARD | XP | ||
| Current position (GPS dependent) | 5 m | 5 m | N/A |
| Attitude (GPS dependent) | 10 m | 10 m | N/A |
| Horizontal Velocities | 0.1 m/s | 0.1 m/s | N/A |
| Vertical Velocity | 0.15 m/s | 0.15 m/s | N/A |
| Attitude (pitch, roll) | 0.85 mR | 0.6 mR | 4 mR |
| True heading (Motion profile dependent) | 2.5 mR | 1.3 mR | 8 mR |
