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Which risk increases when gyroscope sensor data in a quadcopter's flight controller exhibits stochastic resonance?

A)Excessive integral error accumulation
B)Motor desynchronization and burnout
C)Unexpected sharp angular oscillations
D)Propeller blade resonance shattering

💡 Explanation

Unexpected sharp angular oscillations increase because stochastic resonance amplifies noise into periodic-like movements via nonlinear sensor response. Therefore, the controller misinterprets noise as actual rotation corrections, rather than maintaining a stable state under sensor noise suppression.

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