Search Results - "Celani, Fabio"

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  1. 1

    Quaternion versus Rotation Matrix Feedback for Spacecraft Attitude Stabilization Using Magnetorquers by Celani, Fabio

    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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    Journal Article
  2. 2

    Output regulation for the TORA benchmark via rotational position feedback by Celani, Fabio

    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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    Journal Article
  3. 3

    Minimum-Time Spacecraft Attitude Motion Planning Using Objective Alternation in Derivative-Free Optimization by Celani, Fabio, Bruni, Renato

    “…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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    Journal Article
  4. 4

    Robust three-axis attitude stabilization for inertial pointing spacecraft using magnetorquers by Celani, Fabio

    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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    Journal Article
  5. 5

    Global and robust attitude control of a launch vehicle in exoatmospheric flight by Celani, Fabio

    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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    Journal Article
  6. 6

    Gain Selection for Attitude Stabilization of Earth-Pointing Spacecraft Using Magnetorquers by Celani, Fabio

    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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    Journal Article
  7. 7

    Variable-time-domain neighboring optimal guidance and attitude control of low-thrust lunar orbit transfers by Pontani, Mauro, Celani, Fabio

    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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    Journal Article
  8. 8

    Combining Global and Local Strategies to Optimize Parameters in Magnetic Spacecraft Control via Attitude Feedback by Bruni, Renato, Celani, Fabio

    “…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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    Journal Article
  9. 9

    Neighboring Optimal Guidance and Attitude Control of Low-Thrust Earth Orbit Transfers by Pontani, Mauro, Celani, Fabio

    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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    Journal Article
  10. 10

    Neighboring optimal guidance and constrained attitude control applied to three-dimensional lunar ascent and orbit injection by Pontani, Mauro, Celani, Fabio

    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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    Journal Article
  11. 11

    A Robust Optimization Approach for Magnetic Spacecraft Attitude Stabilization by Bruni, Renato, Celani, Fabio

    “…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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    Journal Article
  12. 12

    Lunar descent and landing via two-phase explicit guidance and pulse-modulated reduced-attitude control by Pontani, Mauro, Celani, Fabio, Carletta, Stefano

    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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    Journal Article
  13. 13

    Lunar Ascent and Orbit Injection via Neighboring Optimal Guidance and Constrained Attitude Control by Pontani, Mauro, Celani, Fabio

    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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    Journal Article
  14. 14

    Neighboring Optimal Guidance and Constrained Attitude Control for Accurate Orbit Injection by Pontani, Mauro, Celani, Fabio

    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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    Journal Article
  15. 15

    Crane feedback control in offshore moonpool operations by Messineo, Saverio, Celani, Fabio, Egeland, Olav

    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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    Journal Article
  16. 16
  17. 17

    Spacecraft attitude stabilization with piecewise-constant magnetic dipole moment by Celani, Fabio

    “…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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    Conference Proceeding Journal Article
  18. 18

    Spacecraft Attitude Stabilization with Piecewise-constant Magnetic Dipole Moment by Celani, Fabio

    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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    Journal Article
  19. 19

    Robust Three-axis Attitude Stabilization for Inertial Pointing Spacecraft Using Magnetorquers by Celani, Fabio

    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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    Journal Article
  20. 20

    Omega-limit sets of a class of nonlinear systems that are semiglobally practically stabilized by Byrnes, Christopher I., Celani, Fabio, Isidori, Alberto

    “…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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    Journal Article