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fabio.celani@uniroma1.it
Fabio Celani
Professore Associato
Struttura:
SCUOLA DI INGEGNERIA AEROSPAZIALE
E-mail:
fabio.celani@uniroma1.it
Pagina istituzionale corsi di laurea
Curriculum Sapienza
Pubblicazioni
Titolo
Pubblicato in
Anno
Lunar descent and landing via two-phase explicit guidance and pulse-modulated reduced-attitude control
ACTA ASTRONAUTICA
2023
Reduced-attitude stabilization for spacecraft boresight pointing using magnetorquers
Aeronautics and Astronautics AIDAA XXVII International Congress
2023
Quaternion versus Rotation Matrix Feedback for Spacecraft Attitude Stabilization Using Magnetorquers
AEROSPACE
2022
Explicit Near-Optimal Guidance and Pulse-Modulated Control for Lunar Descent and Touchdown
AEROTECNICA MISSILI E SPAZIO
2022
Correction to: Lunar Descent and Landing via Two-Phase Explicit Guidance and Pulse-Modulated Reduced-Attitude Control
AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
2022
Lunar descent and landing via two-phase explicit guidance and pulse-modulated reduced-attitude control
AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
2022
Robust Collocated Control of Large Flexible Space Structures
IFAC-PapersOnLine
2022
Minimum-Time Spacecraft Attitude Motion Planning Using Objective Alternation in Derivative-Free Optimization
JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS
2021
Explicit near-optimal guidance and pulse-modulated control for lunar descent and touchdown
Proceedings of the XXVI AIDAA International Congress
2021
Neighboring optimal guidance and constrained attitude control for accurate orbit injection
AEROTECNICA MISSILI E SPAZIO
2021
Spacecraft attitude motion planning using gradient-based optimization
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS
2020
Neighboring optimal guidance and attitude control of low-thrust earth orbit transfers
JOURNAL OF AEROSPACE ENGINEERING
2020
Variable-time-domain neighboring optimal guidance and attitude control of low-thrust lunar orbit transfers
ACTA ASTRONAUTICA
2020
Quaternion versus rotation matrix feedback for tigrisat attitude stabilization
Advances in the Astronautical Sciences
2020
Gain Selection for Attitude Stabilization of Earth-Pointing Spacecraft Using Magnetorquers
AEROTECNICA MISSILI E SPAZIO
2020
Combining Global and Local Strategies to Optimize Parameters in Magnetic Spacecraft Control via Attitude Feedback
JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS
2019
Neighboring optimal guidance and constrained attitude control applied to three-dimensional lunar ascent and orbit injection
ACTA ASTRONAUTICA
2019
Spacecraft attitude motion planning on SO(3) using gradient-based optimization
Advances in the Astronautical Sciences
2019
A new guidance and control architecture for accurate orbit injection
Advances in the Astronautical Sciences
2019
Variable-time-domain neighboring optimal guidance and attitude control of low-thrust lunar orbit transfers
Proceedings of the International Astronautical Congress, IAC
2019
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ERC
PE8_1
Keywords
Spacecraft attitude control
Attitude control
nonlinear control
Progetti di Ricerca
Spacecraft Attitude Motion Planning in SO(3)
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