HILS Part Two - Functional Testing

The second part of the HILS was a functional test mainly to observe the functioning of the OpenLog board while the IMU and the servos were running. The logging was set at 38400 bps. The aircraft was moved in pitch, roll and yaw to simulate actual flight. The motor was turned on (without propeller attached) to

Success Criteria
- The logging should not have a loss of data and all IMU and servo variables should be recorded at a rate is for approximately 50hz.

Results:
The figures below show that logging was capable at an approximate rate of 50hz.

This will be tested in the field prior to the first logged flight.

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