Romulus Lungu

Orcid: 0000-0002-3210-4766

Affiliations:
  • University of Craiova, Romania


According to our database1, Romulus Lungu authored at least 18 papers between 2012 and 2023.

Collaborative distances:
  • Dijkstra number2 of five.
  • Erdős number3 of four.

Timeline

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Bibliography

2023
Robust Optimal Control of Spacecraft during the Rendezvous Missions using H∞ Control Method.
Proceedings of the 27th International Conference on System Theory, Control and Computing, 2023

Adaptive Control of the Relative Position for Space Vehicles in the Rendezvous Missions.
Proceedings of the 27th International Conference on System Theory, Control and Computing, 2023

Software And Hardware Platform Using Dynamic Inversion And Neural Networks For The Launch Vehicles.
Proceedings of the 27th International Conference on System Theory, Control and Computing, 2023

Automatic Control of Launch Vehicles' Flight Path Slope Angle by Means of the Backstepping Control Method.
Proceedings of the 9th International Conference on Control, 2023

2020
Backstepping and Dynamic Inversion based Autolanding System for Variable Centre of Mass UAV.
Proceedings of the 24th International Conference on System Theory, Control and Computing, 2020

Backstepping Control of Magnetically Suspended Double-Gimbal Control Moment Gyroscope.
Proceedings of the 24th International Conference on System Theory, Control and Computing, 2020

2019
Adaptive Neural Network-Based Satellite Attitude Control by Using the Dynamic Inversion Technique and a VSCMG Pyramidal Cluster.
Complex., 2019

2018
Neural network based adaptive control of airplane's lateral-directional motion during final approach phase of landing.
Eng. Appl. Artif. Intell., 2018

Reduced-Order Multiple Observer Design for Takagi-Sugeno Models with Unknown Inputs.
Proceedings of the 26th Mediterranean Conference on Control and Automation, 2018

Sliding Mode Control of Launch Vehicles' Flight Path Slope Angle.
Proceedings of the 26th Mediterranean Conference on Control and Automation, 2018

2016
Adaptive flight control law based on neural networks and dynamic inversion for micro-aerial vehicles.
Neurocomputing, 2016

Automatic control of aircraft lateral-directional motion during landing using neural networks and radio-technical subsystems.
Neurocomputing, 2016

Estimation of aircraft state during landing by means of multiple observers.
Proceedings of the International Conference on Systems, Signals and Image Processing, 2016

2015
Determination and Control of the Satellites' Attitude by using a Pyramidal Configuration of Four Control Moment Gyros.
Proceedings of the ICINCO 2015, 2015

2013
Automatic Control of Aircraft in Longitudinal Plane During Landing.
IEEE Trans. Aerosp. Electron. Syst., 2013

Reduced Order Observer for Linear Time-Invariant Multivariable Systems with Unknown Inputs.
Circuits Syst. Signal Process., 2013

2012
Full-order observer design for linear systems with unknown inputs.
Int. J. Control, 2012

Aircrafts state estimation by using an adaptive observer for MIMO linear time varying systems.
Proceedings of the 2012 International Conference on High Performance Computing & Simulation, 2012


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