Fig. 4: Fundamental attributes verification of AET. | Nature Communications

Fig. 4: Fundamental attributes verification of AET.

From: A dexterous and compliant aerial continuum manipulator for cluttered and constrained environments

Fig. 4

“CMD” means commands, “EST” means estimates, and “MEA” means measurements. θu and ϕu denote UAV's attitude. a The actuation mechanism of the continuum arm with essential measurable signals during individual bending motion. b, c, d Limitation evaluation of the bending range, the bending velocity, and the arm tip loading capacity. e Attitude control verification of AET. f Workspace and dexterity maps derivation of the continuum arm.

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