6
Figure 1.5.1: Solo Onboard Sensors Table
*Links to data sheets for sensors listed in this table are location in Appendix 6.4.
1.6 Propulsion
Solo uses four brushless, 880 K
V
motors and four propellers for propulsion. For control and aerodynamic efficiency,
two motors spin clockwise and two motors spin counterclockwise. Navigation in the air is achieved by mixing
propulsion of the four motors to actuate flight control along the roll, pitch, and yaw axes.
Figure 1.6.1: Motor Schematic Diagram
Location
Sensor
Manufacturer / Part Number*
Data Type
Pixhawk 2 FMU
Accelerometer
InvenSense / MPU6000
Orientation
Pixhawk 2 FMU
Gyroscope
InvenSense / MPU6000
Motion
Pixhawk 2 FMU
Magnetometer
Honeywell / HMC 5983
Cardinal direction
Pixhawk 2 FMU
Barometer
Measurement Specialties / MS5611 Altitude
Pixhawk 2 Stabilized IMU
Accelerometer
InvenSense / MPU6000
Orientation
Pixhawk 2 Stabilized IMU
Gyroscope
InvenSense / MPU6000
Motion
Pixhawk 2 Stabilized IMU
Barometer
Measurement Specialties / MS5611 Altitude
Pixhawk 2 Stabilized IMU
Accelerometer
STMicroelectronics / LSM303D
Orientation
Pixhawk 2 Stabilized IMU
Magnetometer
STMicroelectronics / LSM303D
Cardinal direction
Pixhawk 2 Stabilized IMU
Gyroscope
STMicroelectronics / L3GD20
Motion
3DR Solo GPS
GPS
u-blox / NEO-7N
Longitude & latitude
3DR Solo GPS
GPS patch antenna
Taoglas / GP.1575.25.4.A.02
Longitude & latitude
3DR Solo Compass
Magnetometer
Honeywell / HMC 5983
Cardinal direction
Содержание Solo
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