Search Results - "Pontani, M."

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    Near-Optimal Feedback Guidance for Low-Thrust Earth Orbit Transfers by Atmaca, D., Pontani, M.

    Published in Aerotecnica, missili e spazio (01-09-2024)
    “…This research describes a near-optimal feedback guidance, based on nonlinear orbit control, for low-thrust Earth orbit transfers. Lyapunov stability theory…”
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    Journal Article
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    Discrete-Variable-Thrust Guidance for Orbital Rendezvous Based on Feedback Linearization by Napoli, I., Pontani, M.

    Published in Aerotecnica, missili e spazio (01-12-2022)
    “…This research is focused on the analysis, design, and numerical testing of a feedback guidance algorithm for autonomous (unmanned) close-range maneuvering of a…”
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    Journal Article
  4. 4

    Mirror Trajectories in Space Mission Analysis by Pontani, M.

    Published in Aerotecnica, missili e spazio (01-10-2017)
    “…The theorem of mirror trajectories was proven almost six decades ago by Miele, and states that for a given path in the restricted problem of three bodies (with…”
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    Journal Article
  5. 5

    Optimal Mirror Trajectories Using Continuous Thrust by Pontani, M.

    Published in Aerotecnica, missili e spazio (01-10-2017)
    “…The theorem of mirror trajectories, proven almost six decades ago by Miele, states that for a given path in the restricted problem of three bodies (with…”
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    Journal Article
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    A global exploration method to identify families of cycling Earth–Mars trajectories by Fornari, E., Pontani, M.

    Published in Aerotecnica, missili e spazio (01-09-2020)
    “…Cycler mission architectures consider the use of a large space vehicle that cycles continuously between Earth and Mars, describing a near-ballistic path that…”
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    Journal Article
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    Low-Thrust Orbit Dynamics and Periodic Trajectories in the Earth–Moon System by De Leo, L., Pontani, M.

    Published in Aerotecnica, missili e spazio (01-06-2022)
    “…This study employs the circular restricted three-body problem (CR3BP) as the dynamical framework, for the purpose of investigating low-thrust orbit dynamics in…”
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    Journal Article
  8. 8

    A New, General Perturbative Guidance for Space Vehicles by Pontani, M.

    Published in Aerotecnica, missili e spazio (01-04-2016)
    “…Perturbative guidance techniques are aimed at driving a space vehicle along a prescribed, nominal path, leading to fullfilling the boundary conditions…”
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    Journal Article
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    Explicit Near-Optimal Guidance and Pulse-Modulated Control for Lunar Descent and Touchdown by Pontani, M., Celani, F., Carletta, S.

    Published in Aerotecnica, missili e spazio (01-12-2022)
    “…This research considers the descent path of a space vehicle, from periselenium of its operational orbit to the lunar surface. The trajectory is split in two…”
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    Journal Article
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    Optimal Two- and Three-Dimensional Earth–Moon Orbit Transfers by Leonardi, E. M., Pontani, M.

    Published in Aerotecnica, missili e spazio (01-09-2020)
    “…The determination of minimum-propellant-consumption trajectories represents a crucial issue for the purpose of planning robotic and human missions to the Moon…”
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    Journal Article
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    Effect of different flight conditions at the release of a small spacecraft from a high performance aircraft by Ridolfi, L., Pontani, M., Teofilatto, P.

    Published in Acta astronautica (01-03-2010)
    “…In recent years, mainly due to miniaturization of electronics as well as to the improvement of computer performance, small spacecraft have increased their…”
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    Journal Article
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