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
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
Adaptive Neural Network-Based Satellite Attitude Control by Using the Dynamic Inversion Technique and a VSCMG Pyramidal Cluster.
Complex., 2019
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
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
Determination and Control of the Satellites' Attitude by using a Pyramidal Configuration of Four Control Moment Gyros.
Proceedings of the ICINCO 2015, 2015
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
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