Table 5 Steady state error of quadrotor UAV attitude tracking.

From: Trajectory tracking and formation control of quadrotor UAVs based on modified super twisting sliding mode method

 

NTSTSM

STSM

FNTSM

Roll

< 0.01 m

0.1 m

0.02 m

Pitch

< 0.01 m

0.05 m

0.02 m

Yaw

< 0.01 m

< 0.01 m

< 0.01 m

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