Figure7

Reinforcement learning-based attitude control for a quadrotor UAV system with performance constraints

Figure 7. Tracking errors with specified performance under traditional PID control. (A) Attitude tracking error $$ e_{p1} $$; (B) Attitude tracking error $$ e_{p2} $$; (C) Attitude tracking error $$ e_{p3} $$. PID: Proportional-integral-derivative.

Intelligence & Robotics
ISSN 2770-3541 (Online)

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