MEMS INS/GNSS MIG-6000 Series | Tactical-Grade integrated navigation solution

MEMS INS/GNSS MNAV-H01 Series | Tactical-Grade High-Precision integrated-navigation-solution

Compact Structure & Wide Application
The MEMS INS/GNSS MNAV-H01 Series MEMS Inertial/Satellite Integrated Navigation System is a highly reliable, cost-effective 6-axis navigation product, ideal for navigation, control, and measurement in missile-borne platforms, high-dynamic UAVs, unmanned ground vehicles, and unmanned surface vessels.
It integrates high-precision 3-axis MEMS gyroscopes, 3-axis MEMS accelerometers, a dual-antenna GNSS receiver, signal processing circuits, and navigation software, delivering complete navigation and attitude calculation capabilities.

Advanced Manufacturing Processes & Technology
Leveraging leading MEMS processes, the system integrates inertial components with performance comparable to low-precision fiber-optic gyroscopes. Full-temperature parameter compensation (for zero bias, scale factor, non-orthogonal error, etc.) ensures sustained high measurement accuracy over time. An built-in adaptive attitude algorithm guarantees long-term stability in attitude measurements.

Core Self-Aligning Technology
Equipped with high-performance gyroscopes, the system achieves initial north finding without dual-antenna assistance, enabling fast convergence and sustained high accuracy during dynamic navigation.

Key Features

Alternative to fiber-optic grade integrated navigation
Built-in GNSS receiver
Compact size, lightweight, low power consumption
Full-temperature calibration compensation (-45°C to +80°C)
1KHz high-speed sampling
Built-in adaptive Kalman filtering algorithm
Resistant to harsh mechanical environments
Supports online software upgrade

Main Applications

UAVs
Vehicle positioning and heading
Radar/infrared antenna stabilization platforms
Loitering intelligent ammunitions
Port surveying systems
Communication on the Move (COTM)
Attitude reference and control for UAVs, vehicles, ships, and boats
Electro-optical pods
Stabilization and pointing systems

MNAV-H01 Series Performance Specifications
	Parameter Item	MNAV-H01B01	MNAV-H01B05	MNAV-H01B3
Gyroscope	Range (°/s)	±200	±400	±300
	Full-temperature Bias (°/h, 3σ)	≤ 0.3	≤ 2	≤ 80
	Bias Stability (°/h, 10s Smooth)	≤ 0.1	≤ 0.5	≤ 3
	Scale Factor Nonlinearity (ppm)	≤ 100	≤ 100	≤ 100
Accelerometer	Range (g)	±10	±30	±20
	Full-temperature Bias (mg, 3σ)	≤ 0.5	≤ 2	≤ 2
	Bias Stability (μg, 10s Smooth)	≤ 20	≤ 50	≤ 50
	Scale Factor Nonlinearity (ppm)	≤ 100	≤ 100	≤ 100
Navigation Accuracy	North Seeking Accuracy (°, 1σ)	≤ 0.5	≤ 3	/
	Pure Inertial Drift (1σ,60s)	≤ 3m/60s	≤ 5m/60s	≤ 10m/60s
	Combined Horizontal Position (m,1σ)	≤ 2 (Single) ≤0.02+1ppm (RTK)	≤ 2 (Single) ≤0.02+1ppm (RTK)	≤ 2 (Single) ≤0.02+1ppm (RTK)
	Combined Heading Position (m,1σ)	≤ 3 (Single) ≤0.03+1ppm (RTK)	≤ 3 (Single) ≤0.03+1ppm (RTK)	≤ 3 (Single) ≤0.03+1ppm (RTK)
	Combined Horizontal Velocity (m/s,1σ)	≤ 0.05	≤ 0.05	≤ 0.05
	Combined Heading Velocity (m/s,1σ)	≤ 0.1	≤ 0.1	≤ 0.1
	Combined Heading (°,1σ)	≤0.1 (2m Dual Antenna) ≤0.15 (Single Dynamic)	≤0.1 (2m Dual Antenna) ≤0.15 (Single Dynamic)	≤0.1 (2m Dual Antenna) ≤0.2 (Single Dynamic)
	Combined Horizontal Attitude (°,1σ)	≤0.015 (Single Dynamic) ≤0.01 (RTK Dynamic)	≤0.015 (Single Dynamic) ≤0.01 (RTK Dynamic)	≤0.05 (Single Dynamic) ≤0.03 (RTK Dynamic)
Physical Spec	Power Supply (V)	9 ~ 36	9 ~ 36	9 ~ 36
	Static Power (W)	≤ 4	≤ 4	≤ 4
	Start-up Time (s)	≤ 2	≤ 2	≤ 2
	Max Update Rate (Hz)	200	200	200
	Dimensions (mm×mm×mm)	70×66×63	70×66×63	70×66×63
	Weight (g)	370±20	370±20	370±20
Environmental	Operating Temperature (℃)	-40 ~ +80	-40 ~ +80	-40 ~ +80
	Storage Temperature (℃)	-55 ~ +85	-55 ~ +85	-55 ~ +85
	Vibration (g, RMS)	6.06 @ 20~2000Hz	6.06 @ 20~2000Hz	6.06 @ 20~2000Hz
	Shock (g)	500g/1ms	500g/1ms	500g/1ms