Outputs (243)

A conceptual exoskeleton shoulder design for the assistance of upper limb movement (2018)
Presentation / Conference Contribution
Perez, C. N., Georgilas, I., Etoundi, A., Chong, J., & Jafari, A. (2018). A conceptual exoskeleton shoulder design for the assistance of upper limb movement. Lecture Notes in Artificial Intelligence, 10965 LNAI, 291-302. https://doi.org/10.1007/978-3-319-96728-8_25

© Springer International Publishing AG, part of Springer Nature 2018. There is an increased interest on wearable technologies for rehabilitation and human augmentation. Systems focusing on the upper limbs are attempting to replicate the musculoskelet... Read More about A conceptual exoskeleton shoulder design for the assistance of upper limb movement.

Investigation of patterned and non-patterned poly(2,6-dimethyl 1,4-phenylene) oxide based anion exchange membranes for enhanced desalination and power generation in a microbial desalination cell (2018)
Journal Article
Moruno, F. L., Rubio, J. E., Atanassov, P., Cerrato, J. M., Arges, C. G., & Santoro, C. (2018). Investigation of patterned and non-patterned poly(2,6-dimethyl 1,4-phenylene) oxide based anion exchange membranes for enhanced desalination and power generation in a microbial desalination cell. Solid State Ionics, 314, 141-148. https://doi.org/10.1016/j.ssi.2017.11.004

© 2017 The Authors Quaternary ammonium poly(2,6-dimethyl 1,4-phenylene oxide) (QAPPO) anion exchange membranes (AEMs) with topographically patterned surfaces were assessed in a microbial desalination cell (MDC) system. The MDC results with these QAPP... Read More about Investigation of patterned and non-patterned poly(2,6-dimethyl 1,4-phenylene) oxide based anion exchange membranes for enhanced desalination and power generation in a microbial desalination cell.

A New Hydraulic Speed Regulation Scheme: Valve-Pump Parallel Variable Mode Control (2018)
Journal Article
Ding, H., Zhao, J., & Zhu, Q. (2018). A New Hydraulic Speed Regulation Scheme: Valve-Pump Parallel Variable Mode Control. IEEE Access, 6, 55257-55263. https://doi.org/10.1109/ACCESS.2018.2872605

© 2013 IEEE. To improve the comprehensive performances of hydraulic speed regulation systems, this paper proposes and develops a new control scheme, valve-pump parallel variable mode control, which can adopt different control modes in different speed... Read More about A New Hydraulic Speed Regulation Scheme: Valve-Pump Parallel Variable Mode Control.

Negative updating combined with opinion pooling in the best-of-n problem in swarm robotics (2018)
Presentation / Conference Contribution
Lee, C., Lawry, J., & Winfield, A. F. (2018). Negative updating combined with opinion pooling in the best-of-n problem in swarm robotics. Lecture Notes in Artificial Intelligence, 11172 LNCS, 97-108. https://doi.org/10.1007/978-3-030-00533-7_8

© 2018, Springer Nature Switzerland AG. There is a need for effective collective decision making in decentralised multi-agent and robotic systems. This paper introduces a novel approach to the best-of-n decision problem with large n. It utilises nega... Read More about Negative updating combined with opinion pooling in the best-of-n problem in swarm robotics.

Pilot-in-the-loop simulation of flexible aircraft in MATLAB/simulink: Implementation and coding peculiarities (2018)
Presentation / Conference Contribution
Lone, M., Dussart, G., Lopez, G., Lopez Matos, G. E., Portapas, V., Dussart, G. X., …Coetzee, E. (2018). Pilot-in-the-loop simulation of flexible aircraft in MATLAB/simulink: Implementation and coding peculiarities. In 2018 AIAA Modeling and Simulation Technologies Conference. https://doi.org/10.2514/6.2018-0426

© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. Integration of flight dynamic models, developed in the MATLAB®/Simulink® environment, with an engineering flight simulation platform allows rapid pilot-in-the-... Read More about Pilot-in-the-loop simulation of flexible aircraft in MATLAB/simulink: Implementation and coding peculiarities.

Comparison of reduced order aerodynamic models and RANS simulations for whole aircraft aerodynamics (2018)
Presentation / Conference Contribution
Lone, M., Pontillo, A., Dussart, G., Carrizalez, M., Carrizales, M. A., Portapas, V., …Lone, M. M. (2018). Comparison of reduced order aerodynamic models and RANS simulations for whole aircraft aerodynamics. In 2018 AIAA Atmospheric Flight Mechanics Conference. https://doi.org/10.2514/6.2018-0773

© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. Verification and validation of models are critical steps in developing confidence in engineering design processes. The focus of this paper is the verification... Read More about Comparison of reduced order aerodynamic models and RANS simulations for whole aircraft aerodynamics.

The gap of six zeros (2018)
Journal Article
Wright, S. (2018). The gap of six zeros

Passenger drones work in theory, but in order to turn them into the safe, reliable transportation mode of the future, much needs to be done in terms of testing and design.

Control of complex nonlinear dynamic rational systems (2018)
Journal Article
Zhu, Q., Li, L., Zhang, W., & Li, S. (2018). Control of complex nonlinear dynamic rational systems. Complexity, 2018(895303), https://doi.org/10.1155/2018/8953035

© 2018 Quanmin Zhu et al. Nonlinear rational systems/models, also known as total nonlinear dynamic systems/models, in an expression of a ratio of two polynomials, have roots in describing general engineering plants and chemical reaction processes. Th... Read More about Control of complex nonlinear dynamic rational systems.

Analysis of a 3D unsteady morphing wing with seamless side-edge transition (2018)
Presentation / Conference Contribution
Abdessemed, C., Yao, Y., Bouferrouk, A., & Narayan, P. P. (2018). Analysis of a 3D unsteady morphing wing with seamless side-edge transition. In 2018 Applied Aerodynamics Conference. https://doi.org/10.2514/6.2018-3178

© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. In this paper, a comparative study between a NACA 0012 rectangular wing with a statically morphed Trailing Edge Flap (TEF) and the same wing with a hinged flap... Read More about Analysis of a 3D unsteady morphing wing with seamless side-edge transition.

Aerodynamic analysis of a harmonically morphing flap using a hybrid turbulence model and dynamic meshing (2018)
Presentation / Conference Contribution
Abdessemed, C., Yao, Y., Bouferrouk, A., & Narayan, P. P. (2018). Aerodynamic analysis of a harmonically morphing flap using a hybrid turbulence model and dynamic meshing. In 2018 Applied Aerodynamics Conference. https://doi.org/10.2514/6.2018-3813

© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. A numerical study of the NACA 0012 airfoil fitted with a harmonically morphing trailing edge flap (TEF) is performed at an angle of attack of 4º and a Reynolds... Read More about Aerodynamic analysis of a harmonically morphing flap using a hybrid turbulence model and dynamic meshing.