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Hamilton equations are deduced and used for the computation of the theoretical behaviour of this actuator.
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Detailed model of electro servohydraulic actuator based on fluid power engineering is used to emulate the nonlinear behaviour of the actuator.
The closed-loop stability was strongly affected by the dynamic behaviour of the actuator and of the sensor used to measure reaction temperature.
The centerline of this actuator was located at the height of the test anchor.
The built-in strain gauge sensor of this actuator provided a direct reading of the probe's axial displacement.
Unfortunately, the scanning speed of this actuator is limited, and the instrument can only perform en-face (XY-plane) imaging with Z-stack.
The main disadvantages come from the dynamic behaviour of the inertial actuators employed for this application, which are: (i) their low frequency dynamics (that might interact with the structure dynamics), and (ii) their nonlinearities (stroke and force saturation).
The aim of this paper is to describe the behaviour of actuators under load capacity with experimental validation when friction moment is taken into account and becomes an unknown variable.
The present work aims to describe the behaviour of actuators under load capacity with experimental validation.
The behaviour of the large actuators could be predicted accurately with an Arruda-Boyce model and they scale according to theory.
It is well known that the dynamic behaviour of servo-pneumatic actuators depend on the friction force between cylinder and piston, the piston position along the cylinder stroke and the current load due to the high compressibility of air.
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