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Dive into the research topics where Francesco Branz is active.

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Featured researches published by Francesco Branz.


Proceedings of SPIE | 2014

Morphing electroadhesive interface to manipulate uncooperative objects

Livia Savioli; Giovanni Sguotti; Alessandro Francesconi; Francesco Branz; Jeff Krahn; Carlo Menon

The possibility of handling uncooperative objects, i.e. objects not equipped with any features that can aid their manipulation, is of particular interest for both terrestrial and space robotic applications. In this framework, this paper deals with the development and testing of a smart material substrate, which can be integrated into an end-effector device, where morphing and electro-adhesive capabilities are combined to allow the manipulation of uncooperative objects of different shapes and materials. Compliance and adhesion properties are obtained by creating a conductive pattern of electrodes embodied on the surface of a polymeric substrate. On one hand, the polymeric material, activated by a change in temperature, can adapt to any shape when it is heated, and maintain the deformed shape after being cooled, even when the load is removed, becoming compliant with the objects surface. On the other hand, the conductive pattern is responsible for the adhesive effect: when a high voltage is applied, the electric field generated induces an opposite charge on the objects surface establishing reversible attraction forces. Furthermore, the conductive pattern could be used to activate the morphing behaviour when the manipulator and the target object come into contact. A resistiveelectroadhesive pad is realized and some tests are performed to verify the heating behavior of the electrodes and the electroadhesion forces achievable. Morphing tests are also performed to verify the ability of the polymeric substrate to maintain the deformed shape after cooling.


IEEE Transactions on Aerospace and Electronic Systems | 2014

2D Close-Range Navigation Sensor for Miniature Cooperative Spacecraft

Francesco Sansone; Francesco Branz; Alessandro Francesconi; M. Barbetta; M. G. Pelizzo

This paper presents the 2D close-range navigation sensor for cooperative spacecraft developed in the framework of the experiment ARCADE. The sensor exploits an infrared LED transmitter mounted on the target, and two photodiode receivers mounted on the chaser. Laboratory tests were performed to assess the sensor performance and range of application. The accuracies of estimates were, on average, 1.9 mm for distance and 1.0 deg for yaw angle, in ranges of [0.20, 0.42] m and [-40, 40] deg, respectively.


Smart Materials and Structures | 2016

Modelling and control of double-cone dielectric elastomer actuator

Francesco Branz; Alessandro Francesconi

Among various dielectric elastomer devices, cone actuators are of large interest for their multi-degree-of-freedom design. These objects combine the common advantages of dielectric elastomers (i.e. solid-state actuation, self-sensing capability, high conversion efficiency, light weight and low cost) with the possibility to actuate more than one degree of freedom in a single device. The potential applications of this feature in robotics are huge, making cone actuators very attractive. This work focuses on rotational degrees of freedom to complete existing literature and improve the understanding of such aspect. Simple tools are presented for the performance prediction of the device: finite element method simulations and interpolating relations have been used to assess the actuator steady-state behaviour in terms of torque and rotation as a function of geometric parameters. Results are interpolated by fit relations accounting for all the relevant parameters. The obtained data are validated through comparison with experimental results: steady-state torque and rotation are determined at a given high voltage actuation. In addition, the transient response to step input has been measured and, as a result, the voltage-to-torque and the voltage-to-rotation transfer functions are obtained. Experimental data are collected and used to validate the prediction capability of the transfer function in terms of time response to step input and frequency response. The developed static and dynamic models have been employed to implement a feedback compensator that controls the device motion; the simulated behaviour is compared to experimental data, resulting in a maximum prediction error of 7.5%.


Proceedings of SPIE | 2015

Kinematics and control of redundant robotic arm based on dielectric elastomer actuators

Francesco Branz; Andrea Antonello; Andrea Carron; Ruggero Carli; Alessandro Francesconi

Soft robotics is a promising field and its application to space mechanisms could represent a breakthrough in space technologies by enabling new operative scenarios (e.g. soft manipulators, capture systems). Dielectric Elastomers Actuators have been under deep study for a number of years and have shown several advantages that could be of key importance for space applications. Among such advantages the most notable are high conversion efficiency, distributed actuation, self-sensing capability, multi-degree-of-freedom design, light weight and low cost. The big potentialities of double cone actuators have been proven in terms of good performances (i.e. stroke and force/torque), ease of manufacturing and durability. In this work the kinematic, dynamic and control design of a two-joint redundant robotic arm is presented. Two double cone actuators are assembled in series to form a two-link design. Each joint has two degrees of freedom (one rotational and one translational) for a total of four. The arm is designed to move in a 2-D environment (i.e. the horizontal plane) with 4 DoF, consequently having two degrees of redundancy. The redundancy is exploited in order to minimize the joint loads. The kinematic design with redundant Jacobian inversion is presented. The selected control algorithm is described along with the results of a number of dynamic simulations that have been executed for performance verification. Finally, an experimental setup is presented based on a flexible structure that counteracts gravity during testing in order to better emulate future zero-gravity applications.


Proceedings of SPIE | 2014

Design of an innovative Dielectric Elastomer actuator for space applications

Francesco Branz; Francesco Sansone; Alessandro Francesconi

The capability of Dielectric Elastomers to show large deformations under high voltage loads has been deeply investigated to develop a number of actuators concepts. From a space systems point of view, the advantages introduced by this class of smart materials are considerable and include high conversion efficiency, distributed actuation, self-sensing capability, light weight and low cost. This paper focuses on the design of a solid-state actuator capable of high positioning resolution. The use of Electroactive Polymers makes this device interesting for space mechanisms applications, such as antenna and sensor pointing, solar array orientation, attitude control, adaptive structures and robotic manipulators. In particular, such actuation suffers neither wear, nor fatigue issues and shows highly damped vibrations, thus requiring no maintenance and transferring low disturbance to the surrounding structures. The main weakness of this actuator is the relatively low force/torque values available. The proposed geometry allows two rotational degrees of freedom, and simulations are performed to measure the expected instant angular deflection at zero load and the stall torque of the actuator under a given high voltage load. Several geometric parameters are varied and their influence on the device behaviour is studied. Simplified relations are extrapolated from the numerical results and represent useful predicting tools for design purposes. Beside the expected static performances, the dynamic behaviour of the device is also assessed and the input/output transfer function is estimated. Finally, a prototype design for laboratory tests is presented; the experimental activity aims to validate the preliminary results obtained by numerical analysis.


Acta Astronautica | 2013

Active space debris removal by a hybrid propulsion module

Luigi T. DeLuca; F. Bernelli; F. Maggi; P. Tadini; Carmen Pardini; Luciano Anselmo; Michele Grassi; Daniele Pavarin; Alessandro Francesconi; Francesco Branz; Sergio Chiesa; Nicole Viola; C. Bonnal; V. Trushlyakov; Igor Belokonov


63rd International Astronautical Congress 2012, IAC 2012 | 2012

Active space debris removal by hybrid engine module

L.T. De Luca; F. Bernelli; F. Maggi; P. Tadini; Carmen Pardini; Luciano Anselmo; Michele Grassi; Daniele Pavarin; Alessandro Francesconi; Francesco Branz; Sergio Chiesa; Nicole Viola; C. Bonnal; V. Trushlyakov; Igor Belokonov


Ceas Space Journal | 2015

ARCADE-R2 experiment on board BEXUS 17 stratospheric balloon

Marco Barbetta; Alessandro Boesso; Francesco Branz; Andrea Carron; Lorenzo Olivieri; Jacopo Prendin; Gabriele Rodeghiero; Francesco Sansone; Livia Savioli; Fabio Spinello; Alessandro Francesconi


Acta Astronautica | 2014

Active debris multi-removal mission concept based on hybrid propulsion

P. Tadini; Urbano Tancredi; Michele Grassi; Luciano Anselmo; Carmen Pardini; Alessandro Francesconi; Francesco Branz; F. Maggi; Michèle Lavagna; Luigi T. DeLuca; Nicole Viola; Sergio Chiesa; V. Trushlyakov; T. Shimada


ieee international workshop on metrology for aerospace | 2015

Low-cost relative navigation sensors for miniature spacecraft and drones

Francesco Sansone; Alessandro Francesconi; Lorenzo Olivieri; Francesco Branz

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Carmen Pardini

Istituto di Scienza e Tecnologie dell'Informazione

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Luciano Anselmo

Istituto di Scienza e Tecnologie dell'Informazione

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Michele Grassi

University of Naples Federico II

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V. Trushlyakov

Omsk State Technical University

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Urbano Tancredi

University of Naples Federico II

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