Salta al contenuto principale
Ricerc@Sapienza
Toggle navigation
Home
Login
Home
Persone
guido.dematteis@uniroma1.it
Guido De Matteis
Professore Ordinario
Struttura:
DIPARTIMENTO DI INGEGNERIA MECCANICA E AEROSPAZIALE
E-mail:
guido.dematteis@uniroma1.it
Pagina istituzionale corsi di laurea
Curriculum Sapienza
Pubblicazioni
Titolo
Pubblicato in
Anno
Sensor data fusion for precise orbit determination of interplanetary spacecraft
2024
Trajectory Reconstruction of Launch Vehicle in Atmospheric Flight using the Unscented Kalman Filter
AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2023
2023
Optimization of UAV Robust Control Using Genetic Algorithm
IEEE ACCESS
2023
Robust Waypoint Guidance of a Hexacopter on Mars using Meta-Reinforcement Learning
AIAA SciTech Forum and Exposition, 2023
2023
Single axis pointing for underactuated spacecraft with a residual angular momentum
AEROSPACE SCIENCE AND TECHNOLOGY
2022
Estimation of aerodynamic angles and wind components for a launch vehicle
AAS/AIAA Astrodynamics Conference
2022
Optimal tuning for robust control of a small fixed-wing UAV
AIAA Scitech 2021 Forum
2021
Advanced Hinf Synthesis for Launch Vehicle Attitude Control in Atmospheric Flight
AIAA Scitech 2021 Forum
2021
Genetic algorithm based parameter tuning for robust control of launch vehicle in atmospheric flight
IEEE ACCESS
2021
Tracking filter integration in the adaptive augmenting controller of a launch vehicle
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
2021
Optimal tuning of adaptive augmenting controller for launch vehicles in atmospheric flight
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
2020
Adaptive attitude control of launch vehicles in atmospheric flight
2020
Inverse simulation of a helicopter-towing cable-sonar system
ERF european rotorccraft forum
2019
Opportunities and limitations of adaptive augmented control for launch vehicle attitude control in atmospheric flight
2019
Minimum-error single-axis pointing for an underactuated spacecraft in the presence of a residual angular momentum
Proceedings of 69th International Astronautical Congress, IAC
2018
Finite-Element based modeling for flight dynamics and aeroelasticity of flexible aircraft
JOURNAL OF AIRCRAFT
2017
Assessment of helicopter model accuracy through inverse simulation
JOURNAL OF AIRCRAFT
2017
Single-Axis pointing of an underactuated spacecraft equipped with two reaction wheels
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
2017
On the control of aeroelastic/flight dynamic integrated stability of maneuvering aircraft
Proceedings of 17th International forum on aeroelasticity and structural dynamics (IFASD 2017)
2017
Single-axis pointing of underactuated spacecraft with residual angular momentum'
Proceedings of the 6th International Symposium on Space Flight Dynamics
2017
1
2
seguente ›
ultima »
© Università degli Studi di Roma "La Sapienza" - Piazzale Aldo Moro 5, 00185 Roma