CONTROL OF TWO MASS ELECTROMECHANICAL SYSTEM
Journal Title: Engineering and Technology Journal - Year 2018, Vol 3, Issue 6
Abstract
In two-mass electromechanical system, the electromagnetic torque focuses on one (the first) mass. In that case, the second mass related with the first elastic link, can move through oscillating trajectory. The issue of two-mass control system consists of designing the speed regulator that can ensure etalon dynamic processes of second mass movement. A solution to that problem is proposed in this paper.
Authors and Affiliations
BIYA MOTTO Frederic, TCHUIDJAN Roger, NDZANA Benoît
Comparative Study of Source Code Complexity in PHP Web Applications: Utilization of Commercial Code Generators and Manual Framework
This study examined the complexity of source code generated by commercial code generators (PHPMaker and PHPRunner) versus code written manually using the Laravel framework and the open-source code generator CakePHP. Code...
Designing a Data Governance Framework for Cybersecurity Risk Reporting: A Model for Business Intelligence Teams
In the rapidly evolving digital landscape, the integration of robust data governance practices is crucial for enhancing cybersecurity risk reporting within organizations. This abstract presents a model for designing a da...
SUPERLUMINAL PROPAGATION OF PULSE AS ANOTHER ULTRA-FAST PHENOMENON, AND ITS APPLICATION
Another kind of ultra-fast phenomenon, superluminal transmission of light pulse,was proposed, its velocity can faster than the infinite that was proved in theory and experiment. Based on two kinds of epistemology and wo...
Methods of Geological Environment Protection of Luoyang Zhengxingsu Coal Mine
Taking Luoyang Zhengxingsu coal mine as an example, according to the status quo of mine geological environment, the impact assessment of mine geological environment and the protection and management of mine geological en...
Aeroelastic Structural Analysis to Calculate Symmetrical Divergence Modes of an Aircraft Wing Using Aerodynamic Lifting Line Theory
This work explores the use of numerical matrix iteration to determine an aircraft wing's divergence speed using the aerodynamic span effects approach. The present work begins with the construction of equilibrium equation...