Which outcome occurs when an aircraft's fly-by-wire system experiences signal quantization limitations?

💡 Explanation

Increased control surface position dithering results because signal quantization reduces position resolution, driving rapid adjustments via Pulse Width Modulation. This instability is created by a high-frequency limit cycle; therefore, it increases actuator wear compared to smaller oscillations rather than improved component lifetimes.

• Which instability increases when stratified fuel-air mixtures fluctuate in direct injection gasoline engines?
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