Ramy Rashad

Dr. Ramy Rashad


Research Focus & Metrics

Academic Career Length

12Years (2015-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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28 July 2020 in IMA Journal of Mathematical Control and Information
Verified
Journal Article
Open access
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RRRamy Rashad
Ramy Rashad
Federico CalifanoFederico Califano
Federico Califano
ASArjan J van der Schaft
Arjan J van der Schaft
SSStefano Stramigioli
Stefano Stramigioli
The port-Hamiltonian (pH) theory for distributed parameter systems has developed greatly in the past two decades. The theory has been successfully extended from finite-dimensional to infinite-dimensional systems through a lot of research efforts. This article collects the different research studies carried out for distributed pH systems. We classify over a hundred and fifty studies based on different research focuses ranging from modeling, discretization, control and theoretical foundations. This literature review highlights the wide applicability of the pH systems theory to complex systems with multi-physical domains using the same tools and language. We also supplement this article with a bibliographical database including all papers reviewed in this paper classified in their respective groups.

3 February 2020 in IEEE Robotics & Automation Magazine
Verified
Journal Article
Closed access
RRRamy Rashad
Ramy Rashad
JGJelmer Goerres
Jelmer Goerres
RARonald G Aarts
Ronald G Aarts
JEJohan B. C. Engelen
Johan B. C. Engelen
SSStefano Stramigioli
Stefano Stramigioli
RHRamy Hashem
Ramy Hashem

2 August 2019 in IEEE Robotics and Automation Letters
Verified
Journal Article
Closed access
RRRamy Rashad
Ramy Rashad
Federico CalifanoFederico Califano
Federico Califano
SSStefano Stramigioli
Stefano Stramigioli
In this work, we approach the control problem of fully-actuated UAVs in a geometric port-Hamiltonian framework. The UAV is modeled as a floating rigid body on the special Euclidean group SE(3). A unified near-hovering motion and impedance controller is derived by the energy-balancing passivity-based control technique. A detailed analysis of the closed-loop system's behavior is presented for both the free-flight stability and contact stability of the UAV. The robustness of the control system to uncertainties is validated by several experiments, in which the UAV is controlled near its actuator limits. The experiments show the ability of the UAV to hover at its maximum allowed roll angle and apply its maximum allowed normal force to a surface, without the input saturation destabilizing the system.

27 July 2017 in Nonlinear Dynamics
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Journal Article
Closed access
PDF file
AAAhmed Aboudonia
Ahmed Aboudonia
AEAyman El-Badawy
Ayman El-Badawy
RRRamy Rashad
Ramy Rashad

1 July 2017 in ISA Transactions
Verified
Journal Article
Closed access
RRRamy Rashad
Ramy Rashad
AEAyman El-Badawy
Ayman El-Badawy
AAAhmed Aboudonia
Ahmed Aboudonia

1 July 2022 in IEEE Transactions on Robotics
Verified
Journal Article
Closed access
RRRamy Rashad
Ramy Rashad
DBDavide Bicego
Davide Bicego
JZJelle Zult
Jelle Zult
SSSantiago Sanchez-Escalonilla
Santiago Sanchez-Escalonilla
RJRan Jiao
Ran Jiao
SSStefano Stramigioli
Stefano Stramigioli
This work addresses the interaction control problem of a fully actuated aerial vehicle considered as a flying end-effector. We tackle the problem using geometrically consistent variable-stiffness impedance control for safe wrench regulation using the concept of energy tanks, where both the modeling and the control are carried out in the port Hamiltonian framework. We exploit previous well-known results in the literature of ground manipulators and extend them to be applied for novel and challenging aerial physical interaction with a focus on quasi-static applications. The energy-awareness of the presented control method guarantees the stability of the aerial robot in both free-flight and in-contact scenarios together with a level of safety in the case of contact-loss with the unknown environment. Furthermore, by utilizing bond graphs we demonstrate how the closed-loop passivity can be graphically conducted. The validity of our proposed approach is shown via several experiments. We also provide several insights on how the proposed framework could be extended to a generic dynamic aerial physical interaction.