Ruxandra M. Botez
Orcid: 0000-0002-0911-6646Affiliations:
- University of Quebec, Montreal, QC, USA
According to our database1,
Ruxandra M. Botez
authored at least 33 papers
between 2000 and 2024.
Collaborative distances:
Collaborative distances:
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Bibliography
2024
Neural Networks and Support Vector Regression for the CRJ-700 Longitudinal Dynamics Modeling.
J. Aerosp. Inf. Syst., 2024
2023
Performance Model Identification of the General Electric CF34-8C5B1 Turbofan Using Neural Networks.
J. Aerosp. Inf. Syst., 2023
Blockchain PoS and PoW Consensus Algorithms for Airspace Management Application to the UAS-S4 Ehécatl.
Algorithms, 2023
2022
J. Aerosp. Inf. Syst., December, 2022
Performance Improvement of the Regional Jet CRJ700 Aircraft Equipped with Adaptive Winglets.
J. Aerosp. Inf. Syst., October, 2022
Aircraft Mathematical Model Identification for Flight Trajectories and Performance Analysis in Cruise.
J. Aerosp. Inf. Syst., August, 2022
2020
Cessna Citation X Takeoff and Departure Trajectories Prediction in Presence of Winds.
J. Aerosp. Inf. Syst., December, 2020
New Methodology for Aircraft Performance Model Identification for Flight Management System Applications.
J. Aerosp. Inf. Syst., June, 2020
New Adaptive Algorithm Development for Monitoring Aircraft Performance and Improving Flight Management System Predictions.
J. Aerosp. Inf. Syst., February, 2020
2019
Identification and Validation of an Engine Performance Database Model for the Flight Management System.
J. Aerosp. Inf. Syst., August, 2019
2018
Four-Dimensional Aircraft En Route Optimization Algorithm Using the Artificial Bee Colony.
J. Aerosp. Inf. Syst., June, 2018
Aircraft Vertical Route Optimization by Beam Search and Initial Search Space Reduction.
J. Aerosp. Inf. Syst., March, 2018
2017
Four- and Three-Dimensional Aircraft Reference Trajectory Optimization Inspired by Ant Colony Optimization.
J. Aerosp. Inf. Syst., 2017
2015
Flight Trajectory Optimization Through Genetic Algorithms for Lateral and Vertical Integrated Navigation.
J. Aerosp. Inf. Syst., 2015
Methodology for Vertical-Navigation Flight-Trajectory Cost Calculation Using a Performance Database.
J. Aerosp. Inf. Syst., 2015
Tool wear assessment based on type-2 fuzzy uncertainty estimation on acoustic emission.
Appl. Soft Comput., 2015
2014
Type-2 fuzzy tool condition monitoring system based on acoustic emission in micromilling.
Inf. Sci., 2014
Poster abstract: precision improvement of aircrafts attitude estimation through gyro sensors data fusion in a redundant inertial measurement unit.
Proceedings of the IPSN'14, 2014
2013
Redundant Inertial Navigator for Robotic Applications.
Proceedings of the ICINCO 2013 - Proceedings of the 10th International Conference on Informatics in Control, Automation and Robotics, Volume 1, Reykjavík, Iceland, 29, 2013
A redundant aircraft attitude system based on miniaturized gyro clusters data fusion.
Proceedings of Eurocon 2013, 2013
2012
Proceedings of the 38th Annual Conference on IEEE Industrial Electronics Society, 2012
Vertical profile optimization for the Flight Management System CMA-9000 using the golden section search method.
Proceedings of the 38th Annual Conference on IEEE Industrial Electronics Society, 2012
Low-speed aerodynamic characteristics improvement of ATR 42 airfoil using a morphing wing approach.
Proceedings of the 38th Annual Conference on IEEE Industrial Electronics Society, 2012
Proceedings of the 38th Annual Conference on IEEE Industrial Electronics Society, 2012
Proceedings of the 38th Annual Conference on IEEE Industrial Electronics Society, 2012
2010
New Approach for the Identification and Validation of a Nonlinear F/A-18 Model by Use of Neural Networks.
IEEE Trans. Neural Networks, 2010
Morphing Wing Real Time Optimization in Wind Tunnel Tests.
Proceedings of the ICINCO 2010, 2010
Design and Experimental Validation of a Combined PI and Bi-Positional Laws Controller for Delaying the Transition from Laminar Flow to Turbulent Flow over a Morphing Wing.
Proceedings of the Informatics in Control, Automation and Robotics, 2010
A Morphing Wing used Shape Memory Alloy Actuators New Control Technique with Bi-positional and PI Laws Optimum Combination - Part 2: Experimental Validation.
Proceedings of the ICINCO 2010, 2010
A Morphing Wing used Shape Memory Alloy Actuators New Control Technique with Bi-positional and PI Laws Optimum Combination - Part 1: Design Phase.
Proceedings of the ICINCO 2010, 2010
2002
IEEE Trans. Control. Syst. Technol., 2002
Proceedings of the American Control Conference, 2002
2000
H<sub>2</sub> and H<sub>∞</sub>-optimal gust load alleviation for a flexible aircraft.
Proceedings of the American Control Conference, 2000