RESEARCHER PROFILE
Romulus Lungu
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University of Craiova
Romulus Lungu works in Adaptive Control of Nonlinear Systems, Aerospace Engineering and Control Systems, Guidance and Control Systems, Control Systems and Identification, Aerospace and Aviation Technology. Recorded institutional associations include Universitatea Națională de Știință și Tehnologie Politehnica București, University of Craiova.
94Publications
674Citations
15H-index
Inclusion identifies researchers whose recorded research contributions may inform their university’s understanding of its research community. It does not rank individual research quality or establish current employment.
Selected research works
Up to 100 highly cited works; DOI links open the original research. Counts reflect the collected record, not real-time citation totals.
Automatic Control of Aircraft in Longitudinal Plane During Landing
2013 · 66 citationsAutomatic control of aircraft lateral-directional motion during landing using neural networks and radio-technical subsystems
2015 · 49 citationsAdaptive backstepping flight control for a mini‐UAV
2012 · 36 citationsFull-order observer design for linear systems with unknown inputs
2012 · 33 citationsApplication of H 2 /H ∞ and dynamic inversion techniques to aircraft landing control
2015 · 31 citationsAutomatic landing system using neural networks and radio-technical subsystems
2017 · 31 citationsAutomatic Control of Aircraft in Lateral‐Directional Plane During Landing
2015 · 30 citationsReduced Order Observer for Linear Time-Invariant Multivariable Systems with Unknown Inputs
2013 · 27 citationsLanding Auto‐Pilots for Aircraft Motion in Longitudinal Plane using Adaptive Control Laws Based on Neural Networks and Dynamic Inversion
2016 · 27 citationsApplication Of H2/H∞Technique To Aircraft Landing Control
2015 · 24 citationsAutomatic landing control using H-inf control and dynamic inversion
2014 · 23 citationsALSs with Conventional and Fuzzy Controllers Considering Wind Shear and Gyro Errors
2012 · 21 citationsDesign of Full‐Order Observers for Systems with Unknown Inputs by Using the Eigenstructure Assignment
2014 · 21 citationsDesign of Automatic Landing Systems Using the H-inf Control and the Dynamic Inversion
2015 · 21 citationsAdaptive Neural Network‐Based Satellite Attitude Control by Using the Dynamic Inversion Technique and a VSCMG Pyramidal Cluster
2019 · 20 citationsReduced-Order Multiple Observer for Aircraft State Estimation during Landing
2016 · 15 citationsAdaptive control of DGMSCMG using dynamic inversion and neural networks
2021 · 14 citationsNeural network based adaptive control of airplane’s lateral-directional motion during final approach phase of landing
2018 · 13 citationsAttitude adaptive control of satellites using double-gimbal magnetically suspended control moment gyros
2022 · 12 citationsAutonomous Adaptive Control System for Airplane Landing
2018 · 10 citationsAdaptive flight control for a launch vehicle based on the concept of dynamic inversion
2016 · 9 citationsNew Systems for Identification, Estimation and Adaptive Control of the Aircrafts Movement
2011 · 9 citationsDouble-Spool Single Jet Engine for Aircraft as Controlled Object
2008 · 8 citationsDetermination and Control of the Satellites’ Attitude by using a Pyramidal Configuration of Four Control Moment Gyros
2015 · 7 citationsControl of aircraft landing using the dynamic inversion and the H-inf control
2016 · 7 citations
