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M. Bensaada

Researcher at University of Science and Technology of Oran Mohamed-Boudiaf

Publications -  9
Citations -  31

M. Bensaada is an academic researcher from University of Science and Technology of Oran Mohamed-Boudiaf. The author has contributed to research in topics: Spacecraft & Sliding mode control. The author has an hindex of 2, co-authored 7 publications receiving 27 citations.

Papers
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Journal ArticleDOI

A practical design sliding mode controller for DC–DC converter based on control parameters optimization using assigned poles associate to genetic algorithm

TL;DR: In this paper, a simple and systematic approach to design sliding mode controller for buck converters is presented, where the appropriate sliding surface is selected by assigning poles combined with genetic algorithm.
Proceedings ArticleDOI

Sliding mode controller for buck DC-DC Converter

TL;DR: A new control strategy by compromising both schemes advantages and avoiding their drawbacks is proposed, analyzed and simulated.
Journal Article

General Purpose Pulse Width Modulation Based Sliding Mode Controller for Buck DC-DC

TL;DR: In this paper, a simple and systematic approach to the design and analysis of a PWM-based sliding mode controller for buck DC-DC converters is presented, including the practical problems and the proposed solutions.

Solar Arrays and Battery Power Sources Conceptual Design for Low Earth Orbit Microsatellites

TL;DR: In this paper, the authors investigated the power system design trades involved in the mission analysis of a low earth orbit (LEO) satellite at an altitude of 700 km based on the power requirements of the payload and the constant power requirements for the remainder of the spacecraft (platform subsystems).
Journal ArticleDOI

Comparative Analysis of Thermoelectric Generators Parameters

TL;DR: In this paper, a comparative analysis between different commercial thermoelectric generator devices is performed to select the best performance component for a small satellite by exploiting the external thermal properties of the spacecraft on orbit.