Mihai Lungu

Orcid: 0000-0003-1499-0167

According to our database1, Mihai Lungu authored at least 36 papers between 2011 and 2026.

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

Timeline

Legend:

Book  In proceedings  Article  PhD thesis  Dataset  Other 

Links

On csauthors.net:

Bibliography

2026
Improving the Landing Control Capability of Blended Wing Body Configuration Solar-Powered UAVs by Using Swallow Tails and Distributed Propellers.
J. Field Robotics, March, 2026

Curve Virtual Tube Planning and Distributed Control for Swarm UAVs With Complex Constraints and Disturbances.
IEEE Trans. Ind. Electron., February, 2026

Dynamic Event-Triggered Lyapunov-Based Model Predictive Control for AHV Under Disturbance and Multiple Constraints.
IEEE Trans. Circuits Syst. I Regul. Pap., January, 2026

2025
Fault-Tolerant Robust Fast Finite-Time Path-Following Control for Underactuated AUVs With Actuator Dynamics and Saturation.
J. Field Robotics, December, 2025

Distributed Coordinated Control for QUAVs With Switching Formation Strategy.
IEEE Trans. Intell. Veh., June, 2025

Distributed Event-Triggered Collision Avoidance Formation Control for QUAVs With Disturbances Based on Virtual Tubes.
IEEE Trans. Ind. Electron., February, 2025

Decoupled Finite-Time Approximation Auxiliary System-Based Three-Dimensional Integrated Guidance and Control.
IEEE Trans Autom. Sci. Eng., 2025

Dynamic inversion- and neural network- based five-stage cascaded control for automatic carrier landing subject to multiple disturbances and uncertainties.
J. Frankl. Inst., 2025

2024
Antisaturation fixed-time backstepping fuzzy integral sliding mode control for automatic landing of fixed-wing unmanned aerial vehicles.
J. Frankl. Inst., 2024

Dynamic event-triggered fault-tolerant cooperative resilient tracking control with prescribed performance for UAVs.
Sci. China Inf. Sci., 2024

Four-Stage Cascaded Control Scheme Based on Robust Nonlinear Dynamic Inversion Technique for Quadrotors.
Proceedings of the 28th International Conference on System Theory, Control and Computing, 2024

Automatic Attitude Control of the Launch Vehicles by means of the Backstepping Control Method.
Proceedings of the International Conference on Control, Automation and Diagnosis, 2024

2023
Interconnected Disturbance Observer-Based Tracking Control for Permanent Magnet Synchronous Motors.
IEEE Trans. Control. Syst. Technol., November, 2023

Distributed Adaptive Human-in-the-Loop Event-Triggered Formation Control for QUAVs With Quantized Communication.
IEEE Trans. Ind. Informatics, June, 2023

Nonlinear model predictive control of a satellite attitude dynamics in SO(3).
Proceedings of the 27th International Conference on System Theory, Control and Computing, 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

2022
Autonomous Landing of Tailless, Blended Wing, and Variable Centre of Mass UAV using Adaptive Control.
Proceedings of the 8th International Conference on Control, 2022

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

Design of Reduced-Order Multiple Observers for Uncertain Systems with Unknown Inputs.
Complex., 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

2011
Miniature accelerometer precision improvement using intelligent control.
Proceedings of the 6th IEEE International Symposium on Applied Computational Intelligence and Informatics, 2011


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