Single and Dual Antenna GPS-Aided Inertial Navigation Systems (INS)

Product Summary

navigation sensor interface, Inertial Navigation Systems


Dual Antenna
Dual Antenna
 ins heading sensor  gps ins system  magnetic gps inertial navigation system  oem lightweight navigation system dual antenna gps navigation uav
GNSS constellations & corrections GPS L1/L2/L5; GLONASS L1/L2; BeiDou B1/B2/B3; GALILEO E1/E5; SBAS; DGPS; RTK
Position accuracy 1.5 m (GPS L1); 1.2 m (GPS L1/L2); 0.6 m (SBAS); 0.4 m (DGPS); 0.01 m (RTK); 0.005 m (PPK)
GNSS and IMU raw data output YES
Compatible with Pixhawk Autopilot, Embention Autopilot, COBHAM AVIATOR UAV 200, LiDAR, Sonar, Optical Cameras
Input data Marine application: DVL (Doppler Velocity Log)
Land application: Odometer, Wheel sensor, Encoder, DMI
Aerial application: Wind sensor, Air Speed Sensor, Doppler shift from locator (for long-term GPS denied)
Output data Positions, Heading, Dual antenna Heading (D/DL), Pitch, Roll, Velocity, Accelerations, Angular rates,
Barometric data, PPS, Direct AT_ITINS message with Position, Heading, Pitch & Roll to COBHAM AVIATOR UAV 200
Heading accuracy 1 deg (SP)
0.03 deg (PPK)
0.4 deg (SP)
0.03 deg (PPK)
0.05 deg (SP)
0.03 deg (PPK)
Pitch & Roll accuracy 0.1 deg (SP); 0.006 deg (PPK)
IMU Tactical-grade 1 deg /hr Gyroscopes, 0.005 mg accelerometers Bias in-run stability
Size 85 x 47 x 36 mm 120 x 50 x 53 mm 120 x 50 x 53 mm 85 x 47 x 36 mm 120 x 50 x 53 mm
Weight 115 gram 220 gram 280 gram 115 gram 320 gram

GPS-Aided INS Key Performance

Gyroscopes & Accelerometers Bias in-run stability

orientation sensor uav navigation, Inertial Navigation Systems

ins navigation imu sensor, Inertial Navigation Systems

Heading, Pitch & Roll accuracy

yaw pitch roll sensor aerial

The Inertial Labs Single and Dual Antenna GPS-Aided Inertial Navigation System – INS is a new generation of fully-integrated, combined L1 & L2 GPS, GLONASS, GALILEO and BEIDOU navigation and high-performance strapdown system, that determines positions, altitude, velocity, heave and absolute orientation (Heading, Pitch and Roll) for any device on which it is mounted. Horizontal and Vertical Position, Velocity, Heave and Orientation are determined with high accuracy for both motionless and dynamic applications.

The Inertial Labs INS utilizes advanced GNSS receiver, barometer, 3-axes each of calibrated in full operational temperature range precision Fluxgate magnetometers, tactical grade Accelerometers, and Gyroscopes to provide accurate Position, Velocity, Heading, Pitch and Roll of the device under measure.

INS contains Inertial Labs new on-board sensors fusion filter, state of the art navigation and guidance algorithms and calibration software.

Key Features and Functionality Below

Established in 2001, Inertial Labs is a leader in position and orientation technologies for commercial, industrial, aerospace and defense applications. Inertial Labs has a worldwide distributor and representative network covering 20+ countries across 6 continents delivering compact, high performance and affordable Miniature Orientation Sensors, Motion Reference Units (MRU), Attitude & Heading Reference Systems (AHRS) and GPS-Aided Inertial Navigation Systems (INS). With application breadth on Land, Air, and Sea; Inertial Labs covers the gambit of inertial technologies and solutions. Contact us to learn more.