INx1 Inertial Navigation System
INx1 is an advanced GNSS-Assisted Inertial Navigation System (GNSS/INS) that integrates 3-axis gyroscope, accelerometers, magnetometers, a high-sensitivity GNSS receiver, and sophisticated Kalman filtering algorithms to deliver precise assessments of position, velocity, and orientation. INx1 provides accurate navigation, in the event of partial or full loss of GPS due to interference or deliberate jamming.
True Inertial Navigation system:
There are no limitations on mounting orientation or configuration modes; the system offers automatic filter initialization and dynamic alignment.
72 Channel GNSS Receiver:
Equipped with an onboard GNSS receiver that backs GPS, Galileo, and SBAS corrections, this system offers the most compact, high-performance industrial-grade INS available in the market.
Ease of use:
UART or RS232 output for easy integration
True Inertial Navigation system:
There are no limitations on mounting orientation or configuration modes; the system offers automatic filter initialization and dynamic alignment.
72 Channel GNSS Receiver:
Equipped with an onboard GNSS receiver that backs GPS, Galileo, and SBAS corrections, this system offers the most compact, high-performance industrial-grade INS available in the market.
Ease of use:
UART or RS232 output for easy integration
Attitude
Range (Heading/Yaw, Roll) ............................± 180° Range (Pitch) .........................................................± 90° Heading (Magnetic).............................................2.0° RMS Heading (INS)...........................................................0.2°, 1σ Pitch/Roll (Static)....................................................0.5° RMS Pitch/Roll (INS)2 ......................................................0.03°, 1σ Angular Resolution.................................................0.001° GNSS
Receiver Type.......................72 Channel, L1C/A, L1OF, E1, B1I GNSS Constellations......................GPS, GLONASS, Galileo, BeiDou, QZSS Time-To-First-Fix (Cold) ........................30 s Time-To-First-Fix (Hot) .....................................................1 s Altitude Limit .............................................................40,000 m Velocity Limit................................................................500 m/s Communication
Output Data Rate (IMU) ...............................up to 1000 Hz Output Data Rate ............................................up to 500 Hz Data Comm..........................................................RS-232, Serial TTL |
Attitude
Horizontal Position Accuracy ..........................0.5 m RMS Vertical Position Accuracy .................................1.0 m RMS Free Inertial Position Drift ..................................3.0 cm/s2 Velocity Accuracy .....................................................< 0.05 m/s |