GNSS / INS

VN-210

The VN-210 is a tactical-grade, high-performance GNSS-Aided Inertial Navigation System (GNSS/INS) incorporating the latest inertial sensor and GNSS technology. The VN-210 combines a 3-axis accelerometer, a 3-axis gyro, a 3-axis magnetometer, a Multi-band GNSS receiver into a compact embedded module or ruggedized packaging option to deliver a high-accuracy position, velocity and attitude solution.

0.05˚- 0.1˚

Dynamic Heading

0.015˚

Dynamic Pitch/Roll

0.6°/hr

Gyro In-Run Bias

VN-210

The VN-210 is a tactical-grade, high-performance GNSS-Aided Inertial Navigation System (GNSS/INS) incorporating the latest inertial sensor and GNSS technology. The VN-210 combines a 3-axis accelerometer, a 3-axis gyro, a 3-axis magnetometer, and a Multi-band GNSS receiver into a compact ruggedized package to deliver a high-accuracy position, velocity, and attitude solution.

Multi-Band GNSS

Integrated L1/L2/E1/E5b GNSS Receiver

Rugged Device Design

IP-68, DO-160G, MIL-STD-1275E, MIL-STD-461G, MIL-STD-810G

External M-Code

Support for external SAASM / M-Code GPS (ICD-GPS-153)

High Data Rate

400 Hz Navigation Data
800 Hz IMU Data

VN-210 E

The VN-210E is a tactical-grade, high-performance GNSS-Aided Inertial Navigation System (GNSS/INS) incorporating the latest inertial sensor and GNSS technology. The VN-210E combines a 3-axis accelerometer, a 3-axis gyro, a 3-axis magnetometer, and a Multi-band GNSS receiver into a compact embedded module to deliver a high-accuracy position, velocity, and attitude solution.

Multi-Band GNSS

Integrated L1/L2/E1/E5b GNSS Receiver

High Data Rate

400 Hz Navigation Data
800 Hz IMU Data

Ultra-Low SWaP

31 x 31 x 12 mm
14 grams; < 1.5 W

External M-Code

Support for external SAASM / M-Code GPS (ICD-GPS-153)

VN-210 -S

The VN-210-S is a tactical-grade, high-performance GNSS-Aided Inertial Navigation System (GNSS/INS) that combines 3-axis gyros, accelerometers, and magnetometers, a tri-band L1/L2/L5/E1/E5a/b GNSS receiver, and advanced Kalman filtering algorithms to provide optimal estimates of position, velocity, and attitude. The VN-210-S is available in a precision-milled, anodized aluminum enclosure. For ultra-low SWaP applications, the VN-210E (Embedded) can be integrated externally with the GNSS receiver found inside the VN-210-S.

Tri-band GNSS

Integrated L1/L2/L5/E1/E5a/b GNSS Receiver

High Rate Data

400 Hz Navigation Data
800 Hz IMU Data

Ultra Low SWaP

56 x 56 x 31 mm
170 grams; < 3.3 W

Rugged Device Design

Designed to DO-160G, MIL-STD-1275E, MIL-STD-461G, MIL-STD-810G; IP-68 Rated


Specifications

ATTITUDE

Range (Heading/Yaw, Roll)

± 180°

Range (Pitch)

± 90°

Heading (Magnetic)*1

2.0° RMS

Heading (INS)*2

0.05°-0.1°, 1σ

Pitch/Roll (Static)

0.05° RMS

Pitch/Roll (INS)*3

0.015°, 1σ

Heading Mounting Misalignment (VN-210)*4

<0.05°, 1σ

Pitch/Roll Mounting Misalignment*4

<0.05°, 1σ

Angular Resolution

0.001°
POSITION/VELOCITY

Horizontal Position Accuracy*4

1.0 m RMS

Vertical Position Accuracy*4

1.5 m RMS

RTK Position Accuracy*6

0.01m + 1ppm CEP

Free Inertial Position Drift*7

0.5 cm/s²

Velocity Accuracy

< 0.02 m/s
*1With proper magnetic declination, suitable magnetic environment and valid hard/soft iron calibration.
*2Dependant on a number of factors, contact VectorNav to discuss expected performance in your application
*3With sufficient motion for dynamic alignment.
*4Constant on a per part basis. Can be calibrated out during system integration using boresighting or other alignment processes.
*5With SBAS, clear view of GNSS satellites, good multipath environment, compatible GNSS antenna, and as measured over a 24 hour period.
*6Measured using 1km baseline and patch antennas with good ground planes. Does not account for possible antenna phase center offset errors. ppm limited to baselines up to 20km.
*7Typical rate of growth in error of position estimates after loss of GNSS signal, provided INS full alignment prior to loss.

Range

±15 g

In-Run Bias Stability

< 10 μg

Noise Density

< 0.04 mg/√Hz

Bandwidth

200 Hz

Cross-Axis Sensitivity

±0.05°

Range*1

±490°/s (Optional ±2000°/s)

In-Run Bias Stability

< 1°/hr (0.6°/hr typ.)

Noise Density

5°/hr /√Hz

Bandwidth

210 Hz

Cross-Axis Sensitivity

< 0.05°
*1Contact VectorNav for Extended Range Gyro Option

Range

±2.5 Gauss

In-Run Bias Stability

-

Noise Density

140 μGauss/√Hz

Sample Rate

250 HZ

Cross-Axis Sensitivity

±0.05°

Receiver Type

184-Channel, L1/L2/E5b GNSS

Time-to-First-Fix (Cold)

29 s

Time-to-First-Fix (Hot)

1 s

Altitude Limit

50,000 m

Velocity Limit

500 m/s

Size

56 x 56 x 31 mm

Weight

155 g

Interface Connector

Circular Push-Pull Fischer UltiMate (10-pin x 2; Size 7)

GNSS Connector

SMA

Input Voltage

12 to 34 V

Current Draw*1

110mA @ 24 V

Power*1

< 2.7 W

Digital Interface*2

RS-422

Baud Rate

Up to 921,600

GNSS PPS

30ns RMS, 60 ns 99%

Input

Sync-In

Output

Sync-Out
*1 Not including active antenna power consumption.
*2 VN-210: Optional RS-232 on Primary Port

Operating Temperature

-40° to +85° C

Storage Temperature

-40° to +85° C

MTBF

> 21,000 hours

Specifications

Range (Heading/Yaw, Roll)

± 180°

Range (Pitch)

± 90°

Heading (Magnetic)*1

2.0° RMS

Heading (INS)*2

0.05°-0.1°, 1σ

Pitch/Roll (Static)

0.05° RMS

Pitch/Roll (INS)*3

0.015°, 1σ

Heading Mounting Misalignment (VN-210E)*4

0.15°, 1σ

Pitch/Roll Mounting Misalignment*4

<0.05°, 1σ

Angular Resolution

0.001°

Horizontal Position Accuracy*5

2.5 m RMS

Vertical Position Accuracy*5

2.5 m RMS

RTK Position Accuracy*6

0.01m + 1ppm CEP

Free Inertial Position Drift*7

0.5 cm/s2

Velocity Accuracy

< 0.02 m/s
*1With proper magnetic declination, suitable magnetic environment and valid hard/soft iron calibration.
*2Dependant on a number of factors, contact VectorNav to discuss expected performance in your application
*3With sufficient motion for dynamic alignment.
*4Constant on a per part basis. Can be calibrated out during system integration using boresighting or other alignment processes.
*5With SBAS, clear view of GNSS satellites, good multipath environment, compatible GNSS antenna, and as measured over a 24 hour period.
*6Measured using 1km baseline and patch antennas with good ground planes. Does not account for possible antenna phase center offset errors. ppm limited to baselines up to 20km.
*7Typical rate of growth in error of position estimates after loss of GNSS signal, provided INS full alignment prior to loss.

Range

±15 g

In-Run Bias Stability

< 10 μg

Noise Density

0.04 mg/√Hz

Bandwidth

200 Hz

Cross-Axis Sensitivity

±0.05°

Range*1

±490°/s

In-Run Bias Stability

< 1°/hr (0.6°/hr typ.)

Noise Density

5°/hr /√Hz

Bandwidth

210 Hz

Cross-Axis Sensitivity

< 0.05°
*1Contact VectorNav for Extended Range Gyro Option

Range

±2.5 Gauss

In-Run Bias Stability

-

Noise Density

140 μGauss/√Hz

Bandwidth

200 HZ

Cross-Axis Sensitivity

±0.05°

Receiver Type

184-Channel, L1/L2/E5b GNSS

Time-to-First-Fix (Cold)

29 s

Time-to-First-Fix (Hot)

1 s

Altitude Limit

50,000 m

Velocity Limit

500 m/s

Interface Connector

24-pin CLR

GNSS Connector

U. FL

Size

31 x 31 x 12 mm

Weight

14 g

Baud Rate

Up to 921,600

GNSS PPS

30ns RMS, 60 ns 99%

Input

Sync-In

Output

Sync-Out

Input Voltage

3.2 V to 3.5 V

Current Draw*1

280mA @ 3.3 V

Power*1

1 W

Digital Interface

(2) Serial TTL
*1Not including active antenna power consumption.

Operating Temperature

-40° to +85° C

Storage Temperature

-40° to +85° C

MTBF

> 22,000 hours

Specifications

Range (Heading/Yaw, Roll)

± 180°

Range (Pitch)

± 90°

Heading (Magnetic)*1

2.0° RMS

Heading (INS)*2

0.05°-0.1°, 1σ

Pitch/Roll (Static)

0.05° RMS

Pitch/Roll (INS)*3

0.015°, 1σ

Heading Mounting Misalignment*4

<0.05°, 1σ

Pitch/Roll Mounting Misalignment*4

<0.05°, 1σ

Angular Resolution

0.001°

Horizontal Position Accuracy*5

0.6 m RMS

Vertical Position Accuracy*5

0.8 m RMS

RTK Position Accuracy*6

1 cm + 1 ppm CEP

Free Inertial Position Drift*7

0.5 cm/s2

Velocity Accuracy

< 0.02 m/s
*1With proper magnetic declination, suitable magnetic environment and valid hard/soft iron calibration.
*2Dependant on a number of factors, contact VectorNav to discuss expected performance in your application
*3With sufficient motion for dynamic alignment.
*4Constant on a per part basis. Can be calibrated out during system integration using boresighting or other alignment processes.
*5With SBAS, clear view of GNSS satellites, good multipath environment, compatible GNSS antenna, and as measured over a 24 hour period.
*6Dependant on atmospheric conditions, baseline length, GNSS antenna, multipath conditions, satellite visibility and geometry.
*7Typical rate of growth in error of position estimates after loss of GNSS signal, provided INS full alignment prior to loss.

Range

±15 g

In-Run Bias Stability

< 10 μg

Noise Density

< 0.04 mg/√Hz

Bandwidth

200 Hz

Cross-Axis Sensitivity

±0.05°

Range*1

±490°/s (Optional ±2000°/s)

In-Run Bias Stability

< 1°/hr (0.6°/hr typ.)

Noise Density

5°/hr /√Hz

Bandwidth

210 Hz

Cross-Axis Sensitivity

< 0.05°
*1Contact VectorNav for Extended Range Gyro Option

Range

±2.5 Gauss

Noise Density

140 μGauss/√Hz

Sample Rate

250 Hz

Cross-Axis Sensitivity

±0.05°

Receiver Type

448 Channel L1/L2/L5/E1/E5a/b GNSS

Time-To-First-Fix (Cold)

< 45 s

Time-To-First-Fix (Hot)

20 s

Altitude Limit

50,000 m

Velocity Limit

500 m/s

Size

56 x 56 x 31 mm

Weight

170 g

Interface Connector

Circular Push-Pull Fischer UltiMate (10-pin x 2; Size 7)

GNSS Connector

SMA

Baud Rate

Up to 921,00

GNSS PPS

30ns RMS, 60 ns 99%

Input

Sync-In

Output

Sync-Out

Input Voltage

12 to 34 V

Current Draw*1

135 mA @ 24 V

Power*1

< 3.3 W

Digital Interface*2

RS-422
*1Not including active antenna power consumption.
*2VN-210: Optional RS-232 on Primary Port

Operating Temperature

-40° to +85° C

Storage Temperature

-40° to +85° C

Development Kits

VectorNav development kits are built to move fast. Each kit includes the core hardware and interfaces needed to power up quickly, integrate with your system, and validate performance early. Designed for efficient lab and field evaluation, they reduce setup time and integration risk—helping teams confirm fit, functionality, and performance before committing to full deployment.

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