Raw Kinematic Validation Data for Fig. 15 — Folding Angle Tracking of a Cable-Linkage Morphing Flapping-Wing Vehicle (4 Hz)

This dataset contains the theoretical and experimental folding angle trajectories underlying Fig. 15 of the manuscript "Active Load Alleviation of a Falcon-inspired Morphing Flapping-Wing Aerial Vehicle via Cable-Linkage Synergy". The theoretical curve is derived from the closed-loop kinematic constraint model (Eq. 4). The experimental data were captured via an OptiTrack V120:Trio optoelectronic tracking system at 4 Hz flapping frequency over one complete cycle (T = 0.25 s). Column descriptions: Time_t_s (s), Theoretical_Angle_deg (°), Experimental_Angle_deg (°).