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TYF72A-A4L Airborne Fiber-Optic INSHigh-Precision Strapdown and INS-GNSS Integrated Navigation System

TYF72A-A4L Airborne Fiber-Optic INSHigh-Precision Strapdown and INS-GNSS Integrated Navigation System

MOQ: 1
Delivery Period: 60 days
Payment Method: T/T
Detail Information
Place of Origin
China
Model Number
TYF72A-A4L
Highlight:

Airborne Fiber Optic INS

,

Precision Aircraft Inertial Navigation System

Product Description

The device is designed for applications requiring reliable attitude, heading, and position information under demanding dynamic and environmental conditions.
The system is available in two configurations:


General INS (without GNSS)

Integrated INS/GNSS (built-in GNSS receiver)


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


1. 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


2. 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


3. Physical Characteristics

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

4. Electrical & Interface Specifications

Connector: 1 × J30JM-37ZKP43

Includes power input, synchronization, 100 Mbps Ethernet, RS422 serial interfaces

Power Input: 24 VDC (18–36 V)

Power Consumption: ≤ 10 W

Data Output Rate: 200 Hz

Synchronization: Internal sync; external RS422-level sync output


5. System Features

High-stability inertial sensor modules

Supports pure inertial navigation and INS/GNSS integrated navigation

Fast alignment, high output rate (200 Hz)

Robust environmental tolerance: vibration, shock, low temperature

Suitable for long-duration, high-dynamic environments

Standardized electrical interface for easy integration

Products
PRODUCTS DETAILS
TYF72A-A4L Airborne Fiber-Optic INSHigh-Precision Strapdown and INS-GNSS Integrated Navigation System
MOQ: 1
Delivery Period: 60 days
Payment Method: T/T
Detail Information
Place of Origin
China
Model Number
TYF72A-A4L
Minimum Order Quantity:
1
Delivery Time:
60 days
Payment Terms:
T/T
Highlight

Airborne Fiber Optic INS

,

Precision Aircraft Inertial Navigation System

Product Description

The device is designed for applications requiring reliable attitude, heading, and position information under demanding dynamic and environmental conditions.
The system is available in two configurations:


General INS (without GNSS)

Integrated INS/GNSS (built-in GNSS receiver)


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


1. 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


2. 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


3. Physical Characteristics

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

4. Electrical & Interface Specifications

Connector: 1 × J30JM-37ZKP43

Includes power input, synchronization, 100 Mbps Ethernet, RS422 serial interfaces

Power Input: 24 VDC (18–36 V)

Power Consumption: ≤ 10 W

Data Output Rate: 200 Hz

Synchronization: Internal sync; external RS422-level sync output


5. System Features

High-stability inertial sensor modules

Supports pure inertial navigation and INS/GNSS integrated navigation

Fast alignment, high output rate (200 Hz)

Robust environmental tolerance: vibration, shock, low temperature

Suitable for long-duration, high-dynamic environments

Standardized electrical interface for easy integration

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