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Compact and Aircraft Inertial Navigation System with pure inertial and GNSS integrated modes for precise positioning and orientation data

Compact and Aircraft Inertial Navigation System with pure inertial and GNSS integrated modes for precise positioning and orientation data

Nombre De Pièces: 1
Période De Livraison: 60 jours
Méthode De Paiement: T/T
Informations détaillées
Lieu d'origine
Chine
Nom de marque
Wuhan Deep Pilot Technology Co.,Ltd.
Numéro de modèle
TYF51A-A6L
Description du produit

Product Description:

The High-Precision Inertial Navigation System (INS) is a compact, reliable, and versatile navigation solution designed for aerospace, unmanned vehicles, and advanced industrial applications. Featuring both pure inertial and GNSS-integrated modes, it delivers accurate positioning, orientation, and velocity data even in challenging environments where GNSS signals are unreliable.

Key features include fast initial alignment, precise heading, attitude, and velocity measurements, robust environmental adaptability, and user-friendly interfaces for seamless integration. Its aluminum alloy housing ensures efficient heat dissipation, and the modular design allows for easy installation with standardized connectors.

Ideal for composite wing aircraft, target drones, UAVs, and precision-guided systems, this INS is built for high-accuracy navigation and reliable operation under extreme conditions.


Key Features:

  • Fast Alignment: Complete initial alignment in 5 minutes.

  • High Accuracy:

    • Position: 6 nm / 1 h (pure inertial)

    • Heading: 0.1°/h (pure inertial hold)

    • Attitude: 0.05° (pure inertial hold)

    • Velocity: 0.2 m/s (INS/GNSS integrated)

  • Flexible Operation Modes: Pure inertial, GNSS-assisted, or fully integrated navigation.

  • Environmental Adaptability:

    • Operating temperature: -55°C to 70°C, storage: -55°C to 85°C

    • Shock: 20 g, 11 ms, vibration: 6.06 g, 20–2000 Hz

    • Waterproof: IP55

  • Compact & Lightweight: Volume 98 × 96 × 89.5 mm, weight ≤1.3 kg (general model)

  • User Interfaces: RS422 ports, 100 Mbps Ethernet, 24 VDC power supply

  • High-Rate Data Output: Up to 200 Hz navigation data for real-time applications

  • Durable Construction: Aluminum alloy housing with recommended aluminum base for uniform heat dissipation

Specifications Table:

Category Parameter Specification
Performance Alignment Time 5 min

Position Accuracy (RMS) 6 nm / 1 h (pure inertial)
Better than GNSS (INS/GNSS integrated)

Heading Accuracy (RMS) Initial: 0.4° × sec(L)
Pure Inertial Hold: 0.1°/h
INS/GNSS Integrated: 0.2°

Attitude Accuracy (RMS) Pure Inertial Hold: 0.05°
INS/GNSS Integrated: 0.03°

Velocity Accuracy (RMS) INS/GNSS Integrated: 0.2 m/s
Mobility & Environmental Angular Rate Dynamic Range 400 °/s

Acceleration Dynamic Range ±20 g

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

Operating Temperature / Storage -55°C to 70°C / -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

Waterproof Rating IP55
Physical Dimensions (L × W × H) 98 × 96 × 89.5 mm (general)
98 × 96 × 99.5 mm (integrated)

Weight ≤1.3 kg (general)
≤1.5 kg (integrated)
Interfaces Connector 1 × J30JM-25ZKP43 (Power, RS422, Ethernet)

Power Supply 24 VDC (18–36 V), ≤10 W

Data Output Frequency 200 Hz
Installation Mounting 4 × M4 screws, 4 × Φ4.3 mm holes; bottom-mounted recommended; base flatness <0.05 mm

Cable Clearance Tail-out 7.5 mm, recommended 40 mm space for rear cable
Data Output Navigation Data High-rate INS & GNSS navigation data (position, velocity, attitude, heading) with time-stamped messages, RS422 & Ethernet output


produits
DéTAILS DES PRODUITS
Compact and Aircraft Inertial Navigation System with pure inertial and GNSS integrated modes for precise positioning and orientation data
Nombre De Pièces: 1
Période De Livraison: 60 jours
Méthode De Paiement: T/T
Informations détaillées
Lieu d'origine
Chine
Nom de marque
Wuhan Deep Pilot Technology Co.,Ltd.
Numéro de modèle
TYF51A-A6L
Quantité de commande min:
1
Délai de livraison:
60 jours
Conditions de paiement:
T/T
Description du produit

Product Description:

The High-Precision Inertial Navigation System (INS) is a compact, reliable, and versatile navigation solution designed for aerospace, unmanned vehicles, and advanced industrial applications. Featuring both pure inertial and GNSS-integrated modes, it delivers accurate positioning, orientation, and velocity data even in challenging environments where GNSS signals are unreliable.

Key features include fast initial alignment, precise heading, attitude, and velocity measurements, robust environmental adaptability, and user-friendly interfaces for seamless integration. Its aluminum alloy housing ensures efficient heat dissipation, and the modular design allows for easy installation with standardized connectors.

Ideal for composite wing aircraft, target drones, UAVs, and precision-guided systems, this INS is built for high-accuracy navigation and reliable operation under extreme conditions.


Key Features:

  • Fast Alignment: Complete initial alignment in 5 minutes.

  • High Accuracy:

    • Position: 6 nm / 1 h (pure inertial)

    • Heading: 0.1°/h (pure inertial hold)

    • Attitude: 0.05° (pure inertial hold)

    • Velocity: 0.2 m/s (INS/GNSS integrated)

  • Flexible Operation Modes: Pure inertial, GNSS-assisted, or fully integrated navigation.

  • Environmental Adaptability:

    • Operating temperature: -55°C to 70°C, storage: -55°C to 85°C

    • Shock: 20 g, 11 ms, vibration: 6.06 g, 20–2000 Hz

    • Waterproof: IP55

  • Compact & Lightweight: Volume 98 × 96 × 89.5 mm, weight ≤1.3 kg (general model)

  • User Interfaces: RS422 ports, 100 Mbps Ethernet, 24 VDC power supply

  • High-Rate Data Output: Up to 200 Hz navigation data for real-time applications

  • Durable Construction: Aluminum alloy housing with recommended aluminum base for uniform heat dissipation

Specifications Table:

Category Parameter Specification
Performance Alignment Time 5 min

Position Accuracy (RMS) 6 nm / 1 h (pure inertial)
Better than GNSS (INS/GNSS integrated)

Heading Accuracy (RMS) Initial: 0.4° × sec(L)
Pure Inertial Hold: 0.1°/h
INS/GNSS Integrated: 0.2°

Attitude Accuracy (RMS) Pure Inertial Hold: 0.05°
INS/GNSS Integrated: 0.03°

Velocity Accuracy (RMS) INS/GNSS Integrated: 0.2 m/s
Mobility & Environmental Angular Rate Dynamic Range 400 °/s

Acceleration Dynamic Range ±20 g

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

Operating Temperature / Storage -55°C to 70°C / -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

Waterproof Rating IP55
Physical Dimensions (L × W × H) 98 × 96 × 89.5 mm (general)
98 × 96 × 99.5 mm (integrated)

Weight ≤1.3 kg (general)
≤1.5 kg (integrated)
Interfaces Connector 1 × J30JM-25ZKP43 (Power, RS422, Ethernet)

Power Supply 24 VDC (18–36 V), ≤10 W

Data Output Frequency 200 Hz
Installation Mounting 4 × M4 screws, 4 × Φ4.3 mm holes; bottom-mounted recommended; base flatness <0.05 mm

Cable Clearance Tail-out 7.5 mm, recommended 40 mm space for rear cable
Data Output Navigation Data High-rate INS & GNSS navigation data (position, velocity, attitude, heading) with time-stamped messages, RS422 & Ethernet output


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