Search Results - "Celani, Fabio"
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Quaternion versus Rotation Matrix Feedback for Spacecraft Attitude Stabilization Using Magnetorquers
Published in Aerospace (01-01-2022)“…The purpose of this paper is to compare performances between stabilization algorithms of quaternion plus attitude rate feedback and rotation matrix plus…”
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Output regulation for the TORA benchmark via rotational position feedback
Published in Automatica (Oxford) (01-03-2011)“…The present work deals with the design of a feedback controller that solves an output regulation problem for the nonlinear benchmark example known as TORA. The…”
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Minimum-Time Spacecraft Attitude Motion Planning Using Objective Alternation in Derivative-Free Optimization
Published in Journal of optimization theory and applications (01-12-2021)“…This work presents an approach to spacecraft attitude motion planning which guarantees rest-to-rest maneuvers while satisfying pointing constraints. Attitude…”
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Robust three-axis attitude stabilization for inertial pointing spacecraft using magnetorquers
Published in Acta astronautica (01-02-2015)“…In this work feedback control laws are designed for achieving three-axis attitude stabilization of inertial pointing spacecraft using only magnetic torquers…”
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Global and robust attitude control of a launch vehicle in exoatmospheric flight
Published in Aerospace science and technology (01-03-2018)“…The goal of this research is to design global and robust attitude control systems for launch vehicles in exoatmospheric flight. An attitude control system is…”
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Gain Selection for Attitude Stabilization of Earth-Pointing Spacecraft Using Magnetorquers
Published in Aerotecnica, missili e spazio (01-03-2021)“…This paper considers a feedback control law that achieves attitude stabilization for Earth-pointing spacecraft using only magnetorquers as torque actuators…”
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Variable-time-domain neighboring optimal guidance and attitude control of low-thrust lunar orbit transfers
Published in Acta astronautica (01-10-2020)“…Lunar orbit dynamics and transfers at low altitudes are subject to considerable perturbations related to the gravitational harmonics associated with the…”
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Combining Global and Local Strategies to Optimize Parameters in Magnetic Spacecraft Control via Attitude Feedback
Published in Journal of optimization theory and applications (01-06-2019)“…The attitude control of a spacecraft using magnetorquers can be obtained by using attitude feedback, instead of state feedback, with the advantage of not…”
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Neighboring Optimal Guidance and Attitude Control of Low-Thrust Earth Orbit Transfers
Published in Journal of aerospace engineering (01-11-2020)“…AbstractRecently, low-thrust propulsion is gaining strong interest from the research community and has already found application in some mission scenarios…”
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Neighboring optimal guidance and constrained attitude control applied to three-dimensional lunar ascent and orbit injection
Published in Acta astronautica (01-03-2019)“…Future human or robotic missions to the Moon will require efficient ascent path and accurate orbit injection maneuvers, because the dynamical conditions at…”
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A Robust Optimization Approach for Magnetic Spacecraft Attitude Stabilization
Published in Journal of optimization theory and applications (01-06-2017)“…Attitude stabilization of spacecraft using magnetorquers can be achieved by a proportional–derivative-like control algorithm. The gains of this algorithm are…”
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Lunar descent and landing via two-phase explicit guidance and pulse-modulated reduced-attitude control
Published in Acta astronautica (01-11-2023)“…This work considers the three-dimensional descent path of a space vehicle, from periselenium of its operational orbit to the lunar surface. The trajectory is…”
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Lunar Ascent and Orbit Injection via Neighboring Optimal Guidance and Constrained Attitude Control
Published in Journal of aerospace engineering (01-09-2018)“…AbstractFuture human or robotic missions to the Moon will require efficient ascent path and accurate orbit injection maneuvers, because the dynamical…”
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Neighboring Optimal Guidance and Constrained Attitude Control for Accurate Orbit Injection
Published in Aerotecnica, missili e spazio (01-06-2021)“…Accurate orbit injection represents a crucial issue in several mission scenarios, e.g., for spacecraft orbiting the Earth or for payload release from the upper…”
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Crane feedback control in offshore moonpool operations
Published in Control engineering practice (01-03-2008)“…A novel feedback controller for cranes employed in heavy-lift offshore marine operations is proposed. The control objective is to reduce the hydrodynamic…”
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Spacecraft attitude stabilization with piecewise-constant magnetic dipole moment
Published in 2015 7th International Conference on Recent Advances in Space Technologies (RAST) (01-06-2015)“…In actual implementations of magnetic control laws for spacecraft attitude stabilization, the time in which Earth magnetic field is measured must be separated…”
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Spacecraft Attitude Stabilization with Piecewise-constant Magnetic Dipole Moment
Published 15-05-2015“…In actual implementations of magnetic control laws for spacecraft attitude stabilization, the time in which Earth magnetic field is measured must be separated…”
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Robust Three-axis Attitude Stabilization for Inertial Pointing Spacecraft Using Magnetorquers
Published 11-11-2014“…In this work feedback control laws are designed for achieving three-axis attitude stabilization of inertial pointing spacecraft using only magnetic torquers…”
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Omega-limit sets of a class of nonlinear systems that are semiglobally practically stabilized
Published in International journal of robust and nonlinear control (10-05-2005)“…In nonlinear control theory, the equilibrium of a system is semiglobally practically stabilizable if, given two balls centred at the equilibrium, one of…”
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