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TYF72A-A4L – Airborne Fiber-Optic Inertial Navigation System (INS) | High-Precision Strapdown & INS/GNSS Integrated Navigation

TYF72A-A4L – Airborne Fiber-Optic Inertial Navigation System (INS) | High-Precision Strapdown & INS/GNSS Integrated Navigation

MOQ: 1
Price: 1000-10000
Delivery Period: 30 days
Payment Method: T/T,D/P,D/A,L/C
Detail Information
Place of Origin
china
Brand Name
Deep-pilot
Model Number
TYF72A-A4L
Product Description

The TYF72A-A4L is a high-precision airborne fiber-optic inertial navigation system (INS) designed for applications requiring reliable attitude, heading, and position information under demanding dynamic and environmental conditions. It is available in two configurations:

  • General INS (without GNSS)

  • Integrated INS/GNSS (with built-in GNSS receiver)

This system is suitable for UAVs, UGVs, guided weapons, marine platforms, surveying equipment, and other inertial navigation applications.


Performance Specifications

Initial Alignment

  • Alignment Time: 5 minutes

Position Accuracy (CEP)

  • Pure Inertial: 4 nm / 1 hour

  • INS/GNSS Integrated: Better than standalone GNSS positioning accuracy

Heading Accuracy (RMS)

  • Pure Inertial: 0.2° × sec(L), where L is local latitude

  • INS/GNSS Integrated: 0.1°

Attitude Accuracy (Pitch/Roll, RMS)

  • Pure Inertial: 0.03°

  • INS/GNSS Integrated: 0.02°

Velocity Accuracy (RMS)

  • INS/GNSS Integrated: 0.2 m/s


Dynamic & Environmental Capabilities

  • Angular Rate Range: ±400 °/s

  • Acceleration Range: ±20 g

  • Heading / Roll / Pitch Range: Heading 0–360°, Roll ±180°, Pitch ±90°

  • Operating Temperature: –55°C to +70°C

  • Cold Start Temperature: –45°C

  • Storage Temperature: –55°C to +85°C

  • Operating Altitude: 0–20,000 m

  • Vibration: 6.06 g (20–2000 Hz)

  • Shock: 20 g, 11 ms, half-sine

  • Ingress Protection: IP65


Physical Characteristics

Item General INS (No GNSS) Integrated INS/GNSS
Dimensions (L × W × H) 160 × 160 × 115 mm 160 × 160 × 115 mm
Weight ≤ 3.0 kg ≤ 3.3 kg

Electrical & Interface Specifications

  • Connector: 1 × J30JM-37ZKP43 (Power, Synchronization, 100 Mbps Ethernet, RS422)

  • Power Input: 24 VDC (18–36 V)

  • Power Consumption: ≤ 10 W

  • Data Output Rate: 200 Hz

  • Synchronization: Internal sync; external RS422-level sync output


System Features

  • High-stability fiber-optic inertial sensor modules

  • Supports pure inertial navigation and INS/GNSS integrated navigation

  • Fast alignment and high output rate (200 Hz)

  • Robust tolerance to vibration, shock, and low temperature

  • Suitable for long-duration and high-dynamic environments

  • Standardized electrical interface for easy integration

products
PRODUCTS DETAILS
TYF72A-A4L – Airborne Fiber-Optic Inertial Navigation System (INS) | High-Precision Strapdown & INS/GNSS Integrated Navigation
MOQ: 1
Price: 1000-10000
Delivery Period: 30 days
Payment Method: T/T,D/P,D/A,L/C
Detail Information
Place of Origin
china
Brand Name
Deep-pilot
Model Number
TYF72A-A4L
Minimum Order Quantity:
1
Price:
1000-10000
Delivery Time:
30 days
Payment Terms:
T/T,D/P,D/A,L/C
Product Description

The TYF72A-A4L is a high-precision airborne fiber-optic inertial navigation system (INS) designed for applications requiring reliable attitude, heading, and position information under demanding dynamic and environmental conditions. It is available in two configurations:

  • General INS (without GNSS)

  • Integrated INS/GNSS (with built-in GNSS receiver)

This system is suitable for UAVs, UGVs, guided weapons, marine platforms, surveying equipment, and other inertial navigation applications.


Performance Specifications

Initial Alignment

  • Alignment Time: 5 minutes

Position Accuracy (CEP)

  • Pure Inertial: 4 nm / 1 hour

  • INS/GNSS Integrated: Better than standalone GNSS positioning accuracy

Heading Accuracy (RMS)

  • Pure Inertial: 0.2° × sec(L), where L is local latitude

  • INS/GNSS Integrated: 0.1°

Attitude Accuracy (Pitch/Roll, RMS)

  • Pure Inertial: 0.03°

  • INS/GNSS Integrated: 0.02°

Velocity Accuracy (RMS)

  • INS/GNSS Integrated: 0.2 m/s


Dynamic & Environmental Capabilities

  • Angular Rate Range: ±400 °/s

  • Acceleration Range: ±20 g

  • Heading / Roll / Pitch Range: Heading 0–360°, Roll ±180°, Pitch ±90°

  • Operating Temperature: –55°C to +70°C

  • Cold Start Temperature: –45°C

  • Storage Temperature: –55°C to +85°C

  • Operating Altitude: 0–20,000 m

  • Vibration: 6.06 g (20–2000 Hz)

  • Shock: 20 g, 11 ms, half-sine

  • Ingress Protection: IP65


Physical Characteristics

Item General INS (No GNSS) Integrated INS/GNSS
Dimensions (L × W × H) 160 × 160 × 115 mm 160 × 160 × 115 mm
Weight ≤ 3.0 kg ≤ 3.3 kg

Electrical & Interface Specifications

  • Connector: 1 × J30JM-37ZKP43 (Power, Synchronization, 100 Mbps Ethernet, RS422)

  • Power Input: 24 VDC (18–36 V)

  • Power Consumption: ≤ 10 W

  • Data Output Rate: 200 Hz

  • Synchronization: Internal sync; external RS422-level sync output


System Features

  • High-stability fiber-optic inertial sensor modules

  • Supports pure inertial navigation and INS/GNSS integrated navigation

  • Fast alignment and high output rate (200 Hz)

  • Robust tolerance to vibration, shock, and low temperature

  • Suitable for long-duration and high-dynamic environments

  • Standardized electrical interface for easy integration