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Equivalent to Honeywell IMU for Advanced Navigation and Positioning

Produk

Sistem Navigasi Inersia Serat Optik

Sistem Navigasi Inersia Pesawat

Sistem Navigasi Inersia Otomotif

Ring Laser Gyroscope

Hubungi Kami

Miss. Yao

yao@inertial-systems.com

86--18771146215-13212796772

13212796772

Hubungi Sekarang

Equivalent to Honeywell IMU for Advanced Navigation and Positioning

Moq:	1 SET
Harga:	$1000-$100000
Periode pengiriman:	30 hari kerja
metode pembayaran:	T/T
Kapasitas Pasokan:	500 set per tahun

Rincian Informasi

Deskripsi produk

Informasi Rinci

Tempat asal

Nama merek

Star & Inertia Technology

Nomor model

L30 IMU

Waktu startup:

≤ 10 detik (dari penyalaan hingga penyelesaian pengujian mandiri)

Stabilitas bias giroskop:

≤ 0,1°/jam (1σ)

Pengulangan Bias Giroskop:

≤ 0,05°/jam (1σ)

Kesalahan Faktor Skala Giroskop:

≤ 20 ppm (1σ)

Kisaran giroskop:

±1000°/detik

Stabilitas Bias Akselerometer:

≤ 5×10⁻⁵ g (1σ)

Pengulangan Bias Akselerometer:

≤ 5×10⁻⁵ g (1σ)

Kesalahan Faktor Skala Akselerometer:

≤ 50 ppm (1σ)

jangkauan akselerometer:

-60 gram ~ +60 gram

Tingkat Pembaruan Data Navigasi:

≥ 200Hz

Tegangan Masukan:

18–32 V, tipikal 24 V

Konsumsi Daya (Kondisi Mantap):

≤ 15W

Berat:

≤ 1,5kg

Dimensi (L × T):

110mm × 115mm

Antarmuka:

1×RS232, 1×RS485, 1×RS422

Suhu Operasional:

-40 °C ~ +60 °C

Suhu Penyimpanan:

-55 °C ~ +70 °C

Kelembaban Pengoperasian:

≤ 95% (25 °C)

Kelembaban penyimpanan:

≤ 95% (30 °C)

Deskripsi produk

The next-generation gyrocompassing-grade Inertial Measurement Unit (IMU) is engineered for demanding navigation and precision positioning applications. Designed for mission-critical platforms, it delivers high-accuracy heading, attitude, and inertial navigation performance for aerospace, defense, unmanned systems, industrial surveying, and maritime operations.

The unit integrates advanced inertial sensing architecture within a rugged, environmentally-sealed aluminum enclosure, providing exceptional resistance to vibration, shock, and harsh environmental conditions. It maintains long-term performance stability without the need for external cooling or auxiliary thermal management.

This IMU is deployed across a wide range of platforms and operational environments, including:

UAV/VTOL flight control and navigation
UGV/USV/UUV autonomous navigation
Weapon stabilization and targeting
Maritime surveying and subsea exploration
Industrial drilling navigation and ground surveying
High-precision mapping & GIS platforms
Aerospace inertial navigation and GNSS-denied operations

Multiple interface and output configurations are available to support flexible integration into flight control computers, navigation computers, GNSS/INS integrated solutions, and avionics architectures. Users can configure output data rates, filtering modes, and communication protocols to optimize performance for specific mission profiles.

As a gyrocompassing-class inertial sensor, the unit offers high stability, high reliability, and excellent SWaP (Size, Weight, and Power) characteristics — providing advanced inertial navigation capability with reduced system burden. It is well-suited for applications requiring high-precision heading, inertial positioning, and sustained autonomy in GPS-denied or contested environments.

Parameter	Specification
Navigation System	Strapdown Inertial System (SINS)
Startup Time	≤ 10 s (from power-on to self-test completion)
Core Sensor Accuracy – Gyroscope	Bias stability: ≤ 0.1°/h (1σ)
	Bias repeatability: ≤ 0.05°/h (1σ)
	Scale factor error: ≤ 20 ppm (1σ)
	Random walk: ≤ 0.02°/√h (1σ)
	Range: ±1000°/s
Core Sensor Accuracy – Accelerometer	Bias stability: ≤ 5×10⁻⁵ g (1σ)
	Bias repeatability: ≤ 5×10⁻⁵ g (1σ)
	Scale factor error: ≤ 50 ppm (1σ)
	Range: -60 g ~ +60 g
Navigation Data Update Rate	≥ 200 Hz
Input Voltage	18–32 V, typical 24 V
Power Consumption (Steady-State)	≤ 15 W
Weight	≤ 1.5 kg
Dimensions (D × H)	110 mm × 115 mm
Interfaces	1 × RS232, 1 × RS485, 1 × RS422
Operating Temperature	-40 °C ~ +60 °C
Storage Temperature	-55 °C ~ +70 °C
Operating Humidity	≤ 95% (25 °C)
Storage Humidity	≤ 95% (30 °C)

Produk

Moq:	1 SET
Harga:	$1000-$100000
Periode pengiriman:	30 hari kerja
metode pembayaran:	T/T
Kapasitas Pasokan:	500 set per tahun

Informasi Rinci

Deskripsi produk

Informasi Rinci

Tempat asal

Nama merek

Star & Inertia Technology

Nomor model

L30 IMU

Waktu startup:

≤ 10 detik (dari penyalaan hingga penyelesaian pengujian mandiri)

Stabilitas bias giroskop:

≤ 0,1°/jam (1σ)

Pengulangan Bias Giroskop:

≤ 0,05°/jam (1σ)

Kesalahan Faktor Skala Giroskop:

≤ 20 ppm (1σ)

Kisaran giroskop:

±1000°/detik

Stabilitas Bias Akselerometer:

≤ 5×10⁻⁵ g (1σ)

Pengulangan Bias Akselerometer:

≤ 5×10⁻⁵ g (1σ)

Kesalahan Faktor Skala Akselerometer:

≤ 50 ppm (1σ)

jangkauan akselerometer:

-60 gram ~ +60 gram

Tingkat Pembaruan Data Navigasi:

≥ 200Hz

Tegangan Masukan:

18–32 V, tipikal 24 V

Konsumsi Daya (Kondisi Mantap):

≤ 15W

Berat:

≤ 1,5kg

Dimensi (L × T):

110mm × 115mm

Antarmuka:

1×RS232, 1×RS485, 1×RS422

Suhu Operasional:

-40 °C ~ +60 °C

Suhu Penyimpanan:

-55 °C ~ +70 °C

Kelembaban Pengoperasian:

≤ 95% (25 °C)

Kelembaban penyimpanan:

≤ 95% (30 °C)

Kuantitas min Order:

1 SET

Harga:

$1000-$100000

Waktu pengiriman:

30 hari kerja

Syarat-syarat pembayaran:

Menyediakan kemampuan:

500 set per tahun

Deskripsi produk

This IMU is deployed across a wide range of platforms and operational environments, including:

UAV/VTOL flight control and navigation
UGV/USV/UUV autonomous navigation
Weapon stabilization and targeting
Maritime surveying and subsea exploration
Industrial drilling navigation and ground surveying
High-precision mapping & GIS platforms
Aerospace inertial navigation and GNSS-denied operations

Parameter	Specification
Navigation System	Strapdown Inertial System (SINS)
Startup Time	≤ 10 s (from power-on to self-test completion)
Core Sensor Accuracy – Gyroscope	Bias stability: ≤ 0.1°/h (1σ)
	Bias repeatability: ≤ 0.05°/h (1σ)
	Scale factor error: ≤ 20 ppm (1σ)
	Random walk: ≤ 0.02°/√h (1σ)
	Range: ±1000°/s
Core Sensor Accuracy – Accelerometer	Bias stability: ≤ 5×10⁻⁵ g (1σ)
	Bias repeatability: ≤ 5×10⁻⁵ g (1σ)
	Scale factor error: ≤ 50 ppm (1σ)
	Range: -60 g ~ +60 g
Navigation Data Update Rate	≥ 200 Hz
Input Voltage	18–32 V, typical 24 V
Power Consumption (Steady-State)	≤ 15 W
Weight	≤ 1.5 kg
Dimensions (D × H)	110 mm × 115 mm
Interfaces	1 × RS232, 1 × RS485, 1 × RS422
Operating Temperature	-40 °C ~ +60 °C
Storage Temperature	-55 °C ~ +70 °C
Operating Humidity	≤ 95% (25 °C)
Storage Humidity	≤ 95% (30 °C)

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Ring Laser Gyroscope

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Unit Pengukuran Inersia MEMS