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Kalman Filter GNSS Strapdown Aircraft Inertial Navigation System FOG INS SMALL

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

Kalman Filter GNSS Strapdown Aircraft Inertial Navigation System FOG INS SMALL

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

Cina

Nama merek

Star & Inertia Technology

Waktu penyelarasan:

≤5 menit

Akurasi posisi/inersia murni:

5m/60s (ref.), 150m/300s (ref.), Cep

Kombinasi Akurasi Posisi/Navigasi Inersia:

Lebih baik dari akurasi satelit

Akurasi kecepatan/inersia murni:

——

Kombinasi Akurasi Kecepatan/Navigasi Inersia:

≤0,2m/detik

Akurasi heading/inersia murni:

≤0,5 ° SECL+0,1 °/jam, RMS

Kombinasi Navigasi Akurasi/Satelit:

≤0,3°

Akurasi pitch & roll/inersia murni:

≤0,1°

Kombinasi Navigasi Akurasi/Satelit Pitch & Roll:

≤0,05°

Ukuran:

100 × 100 × 90mm

Berat:

< 1,5 kg

Suhu:

-40 ℃ ~ 60 ℃

Tegangan Masukan:

DC24V (± 25%)

Menyoroti:

GNSS ins inertial navigation system

SMALL ins inertial navigation system

SMALL inertial navigation unit

Deskripsi produk

Delivering exceptional navigation performance, this fiber-optic inertial navigation system (FOG INS) integrates FOG/RLG gyroscopes and quartz accelerometers in a strapdown configuration. Its real-time sensor fusion engine combines inertial data with GNSS, celestial, and other navigation sources, ensuring accurate and reliable positioning even in GPS-denied environments.

Key Advantages for UAV Applications

Reliable ground and air alignment for rapid mission readiness
Multiple alignment mode selection for flexible deployment
Scalable navigation augmentation with multi-source integration
Continuous system monitoring for enhanced operational reliability

Series			FOG INS
Accelerometer	Months Bias Repeatability(1σ)		≤100μg
	Months Scale Factor Accuracy(1σ)		≤100ppm
Gyro	Bias Repeatability(1σ)		≤0.05°/hr
	Scale Factor Accuracy(1σ)		≤100ppm
	Random walk(1σ)		≤0.02°/√hr
Features	Position Accuracy	Pure inertia	5m/60s(Ref.),150m/300s(Ref.),CEP
		Inertial navigation satellite combination	better than satellite accuracy
	Speed Accuracy	Pure inertia	——
		Inertial navigation satellite combination	≤0.2m/s,RMS
	Angular Rate		≥±400°/sec
	Angular Acceleration		100000°/sec2
	Acceleration		＞25g
	Angular Attitude		Any Orientation
	Input/output		3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time			＜5min
AHRS Applications Performance	Heading Accuracy	Pure inertia	≤0.5°secL+0.1°/h,RMS
		Satellite navigation combination	≤0.3°,RMS
	Pitch & Roll Accuracy	Pure inertia	≤0.1°,RMS
		Satellite navigation combination	≤0.05°,RMS
Characteristics	Power consumption		＜15W
	Dimensions		100×100×90
	Weight		＜1.5kg
	Temperature		-40℃~60℃
	Shock		15g,Half-sine wave 11ms
	Input Voltage		DC24V(±25%)
	cooling		Conduction to mounting plate
	Vibration		20~2000Hz,6.06g
	MTBF		＞20000 hours

Tag:

Sistem inersia strapdown,

Sistem navigasi inersia kabut,

FOG INS

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Unit Pengukuran Inersia IMU

Giroskop serat optik

Ring Laser Gyroscope

Kalman Filter GNSS Strapdown Aircraft Inertial Navigation System FOG INS SMALL

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

Cina

Nama merek

Star & Inertia Technology

Waktu penyelarasan:

≤5 menit

Akurasi posisi/inersia murni:

5m/60s (ref.), 150m/300s (ref.), Cep

Kombinasi Akurasi Posisi/Navigasi Inersia:

Lebih baik dari akurasi satelit

Akurasi kecepatan/inersia murni:

——

Kombinasi Akurasi Kecepatan/Navigasi Inersia:

≤0,2m/detik

Akurasi heading/inersia murni:

≤0,5 ° SECL+0,1 °/jam, RMS

Kombinasi Navigasi Akurasi/Satelit:

≤0,3°

Akurasi pitch & roll/inersia murni:

≤0,1°

Kombinasi Navigasi Akurasi/Satelit Pitch & Roll:

≤0,05°

Ukuran:

100 × 100 × 90mm

Berat:

< 1,5 kg

Suhu:

-40 ℃ ~ 60 ℃

Tegangan Masukan:

DC24V (± 25%)

Kuantitas min Order:

1 set

Harga:

$1000-$100000

Waktu pengiriman:

30 hari kerja

Syarat-syarat pembayaran:

T/T

Menyediakan kemampuan:

500 set per tahun

Menyoroti

GNSS ins inertial navigation system

SMALL ins inertial navigation system

SMALL inertial navigation unit

Deskripsi produk

Key Advantages for UAV Applications

Reliable ground and air alignment for rapid mission readiness
Multiple alignment mode selection for flexible deployment
Scalable navigation augmentation with multi-source integration
Continuous system monitoring for enhanced operational reliability

Series			FOG INS
Accelerometer	Months Bias Repeatability(1σ)		≤100μg
	Months Scale Factor Accuracy(1σ)		≤100ppm
Gyro	Bias Repeatability(1σ)		≤0.05°/hr
	Scale Factor Accuracy(1σ)		≤100ppm
	Random walk(1σ)		≤0.02°/√hr
Features	Position Accuracy	Pure inertia	5m/60s(Ref.),150m/300s(Ref.),CEP
		Inertial navigation satellite combination	better than satellite accuracy
	Speed Accuracy	Pure inertia	——
		Inertial navigation satellite combination	≤0.2m/s,RMS
	Angular Rate		≥±400°/sec
	Angular Acceleration		100000°/sec2
	Acceleration		＞25g
	Angular Attitude		Any Orientation
	Input/output		3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time			＜5min
AHRS Applications Performance	Heading Accuracy	Pure inertia	≤0.5°secL+0.1°/h,RMS
		Satellite navigation combination	≤0.3°,RMS
	Pitch & Roll Accuracy	Pure inertia	≤0.1°,RMS
		Satellite navigation combination	≤0.05°,RMS
Characteristics	Power consumption		＜15W
	Dimensions		100×100×90
	Weight		＜1.5kg
	Temperature		-40℃~60℃
	Shock		15g,Half-sine wave 11ms
	Input Voltage		DC24V(±25%)
	cooling		Conduction to mounting plate
	Vibration		20~2000Hz,6.06g
	MTBF		＞20000 hours

Tag: