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Table 1 Proportional-integral-derivative parameter

From: Simulating unmanned aerial vehicle flight control and collision detection

Gesture of unmanned aerial vehicle Proportional P Integral I Differential D
Pitch angle 2.7 0.03 0.75
Roll angle 2.8 0.04 0.80
Yaw angle 4.4 0.06 1.50
Height 3.0 0.08 1.25
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