The center of gravity (CG) is a critical factor in aviation, affecting the aircraft’s stability and handling characteristics. The autopilot system requires the CG to be within a specific range for optimal performance.
The CG limit for an autopilot system can be calculated using the formula:
Wfwd = Weight forward of the CG limit
Waft = Weight aft of the CG limit
Maintaining the CG within this range ensures that the autopilot can effectively control the aircraft.
What is the formula for calculating CG limit?
Why is maintaining CG within a specific range important?
How does weight distribution affect CG limit?
Can I use this calculator for any aircraft type?
What happens if the CG goes beyond the limit?
Is there a way to adjust the CG once it’s out of range?
Can this calculator help prevent stalls during flight?
Results are for informational purposes only and do not constitute professional advice.
