The loose combination adopts two independent systems, inertial navigation system and satellite receiver system.The error equation of inertial navigation is used as the system equation, and the difference between the position and velocity of inertial navigation output and that of satellite receiver is used as the quantity measurement of the system.Then, the attitude error, position error and velocity error of the Kalman filter are used to update the position, speed and attitude of the inertial navigation output.
- North Seeker
- Gyro Sensor
- Accelerometer
- IMU
- INS
- AHRS
- Positioning & Orientation System
- Logging Tools/Gyro Tools
- Inertial Geodetic Survey System
- Gyrocompass
- Gyro Theodolite
- Inertial Testing Device
- GNSS Antenna
- GNSS Module
- GNSS Board
- Satellite Receiver
- Satellite Handheld Device
- Satellite Signal Simulator
- Anti UAV Defence System
- Electrical Motor
- Pressure Sensors
- Tilt Sensor
- Digital Compass
- Acceleration Sensor
- Tilt Switch
- Angle Sensor
- Digital Display Tilt Sensor
- Power Supply
- Robot Joint Reducer
- Industrial Intelligentization System
APPLICATION