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Which outcome results when excessive proportional integral derivative (PID) gain destabilizes a drone's gyroscope?

A)Oscillatory attitude and control hunting
B)Reduced control signal quantization error
C)Improved steady-state motor output
D)Damped response to environmental changes

💡 Explanation

Oscillatory attitude occurs because excessive PID gain amplifies sensor noise through positive feedback in the control loop (gain too high); therefore the drone attitude oscillates, rather than provide stable hovering, even with small disturbances.

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