Dynon Avionics D1 - Manual (Page 15)

D1 Pilot’s User Guide 4-1
4. PRODUCT TOUR
On-Screen Elements
Aircraft Attitude is determined by combining information from internal solid state rotation rate
sensors (gyros) and accelerometers. GPS information is additionally used to ensure the quality of
the displayed attitude indication. When properly aligned to the aircraft, the D1’s attitude will
perform as well or better than a conventional mechanical gyro-based attitude indicator.
Figure 1- Full D1 Display with Attitude