Attitude Heading Reference System:
Inertial Sensor providing following Informations:
- Relative Position Pitch, Roll, Yaw: deg
- Angular Rates above all axis (): deg/s
- Accelerations (X/Y/Z): m/s^2
- Gravity vector (X/Y/Z): g
Attitude Heading Reference System:
Inertial Sensor providing following Informations:
- Relative Position Pitch, Roll, Yaw: deg
- Angular Rates above all axis (): deg/s
- Accelerations (X/Y/Z): m/s^2
- Gravity vector (X/Y/Z): g
Sampling Rate: up to 500Hz
Interface: User Selectable
- CAN Bus (CanAerospace Protocol)
- RS232
- RS485
- I2C
Power:
- Voltage: 9-36VDC
- Consumption max. 200mA