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Navigation Grade MEMS IMU with 3 Axis Accelerometer Gyroscope

Наименование марки:	FIREPOWER
Номер модели:	ИМУ6-4
МОК:	1
Условия оплаты:	Л/К, Т/Т, западное соединение
Способность к поставкам:	500/месяц

Подробная информация

Описание продукта

Подробная информация

Место происхождения:

Китай

Масса:

55±5 г

Диапазон измерения:

± 400 °/с

Нестабильность при нулевом смещении:

1°/ч

Случайная прогулка:

0,15。/√ч

Повторяемость с нулевым смещением:

10°/h

Чувствительность ускорения при нулевом смещении:

1°/h/g

Нелинейность масштабного коэффициента:

300 млрд

Пропускная способность:

250hz

Упаковывая детали:

губка + коробка

Поставка способности:

500/месяц

Выделить:

navigation grade MEMS IMU sensor

3 axis accelerometer gyroscope

MEMS IMU with gyroscope

Описание продукта

Navigation Grade MEMS IMU with 3-Axis Accelerometer & Gyroscope

Composition and Function

The inertial measurement unit integrates multiple precision sensors and processing components:

Three-axis gyroscope for angular rate measurement
Three-axis accelerometer for acceleration measurement
Three-axis tilt angle sensor (optional)
Temperature sensor for environmental compensation
Signal processing board with advanced algorithms
Robust mechanical structure
Comprehensive software suite

The system measures three-axis angular rate, acceleration, and tilt angle of the carrier, then outputs compensated data (including temperature compensation, installation misalignment compensation, and nonlinear compensation) through an RS-422 serial port using standardized communication protocols.

Gyroscope Technical Specifications

Parameter	Unit	Test Conditions	IMU6-4	IMU6-4A	IMU6-4B	IMU6-4C
Measuring range	°/s		±400	±400	±400	±2000
Zero-bias instability	°/h	Allan variance	1	0.1	0.05	3
Zero bias stability	°/h	1s smooth, RMS, normal temperature	10	5	1	20
Zero bias variation at full temperature	°/h	10s smooth, RMS, temperature change rate 1 ℃/min	20	10	2	40
Random walk	./√h	Allan variance	0.15	0.05	0.02	0.3
Zero-bias repeatability	°/h	Q = 6, normal temperature	10	5	1	20
Zero bias acceleration sensitivity	°/h/g	Test at ± 1 g	1	1	1	1
Resolution	°/h		2	1	0.5	5
Output noise	°/s	Peak (half peak, STD * 3)	0.3	0.25	0.15	0.45
Scale factor nonlinearity	ppm	Normal temperature	300
Scale factor repeatability	ppm	Q = 3, normal temperature	300
Cross coupling	%	Normal temperature	0.2
Bandwidth	Hz		250	250	150	250

Accelerometer Technical Specifications

Parameter	Unit	Test Conditions	IMU6-4y-1	IMU6-4y-2	IMU6-4y
Measuring range	g		±10	±20	±40
Zero bias stability	mg	1s smooth, RMS, normal temperature	0.1	0.2	0.3
Zero bias variation at full temperature	mg	10s smooth, RMS, temperature change rate 1 ℃/min	3	3	5
Zero-bias repeatability	mg	Q = 6, normal temperature	0.2	0.5	1
Resolution	mg		0.1	0.1	0.1
Scale factor nonlinearity	ppm	Normal temperature	500
Scale factor repeatability	ppm	Q = 3, normal temperature	500
Cross coupling	%	Normal temperature	0.2
Bandwidth	Hz		150