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        Removing energy from a spacecraft using tethers 

        Universidade Estadual Paulista (Unesp); INPE (2019-01-01)
        For a mission whose focus is the capture of the spacecraft by the main body or a close approach for observation, removing energy from a spacecraft can be an important maneuver. An option is the Tethered Slingshot Maneuver ...

        An interplanetary mission to Neptune system: Gravitational capture and maneuvers around triton 

        Instituto Nacional de Pesquisas Espaciais (INPE); Universidade Estadual Paulista (Unesp) (2007-12-01)
        The gravitational capture was initially used to understand the capture of planetary satellites. However, in the 90's decade, this phenomenon was applied in spacecraft trajectories. Belbruno and Miller studied missions in ...

        An interplanetary mission to Neptune system: Gravitational capture and maneuvers around triton 

        Instituto Nacional de Pesquisas Espaciais (INPE); Universidade Estadual Paulista (Unesp) (2007-12-01)
        The gravitational capture was initially used to understand the capture of planetary satellites. However, in the 90's decade, this phenomenon was applied in spacecraft trajectories. Belbruno and Miller studied missions in ...

        An interplanetary mission to Neptune system: Gravitational capture and maneuvers around triton 

        Solórzano, Carlos Renato Huaura; De Almeida Prado, Antonio Fernando Bertachini; Winter, Othon Cabo (2014)

        Attitude stabilization of a rigid spacecraft in the geomagnetic field 

        Natl Res Inst Astron & Geophys Helwan; Universidade Estadual Paulista (Unesp) (Elsevier B.V., 2007-01-01)
        An analytical method is proposed to study the attitude stability of a triaxial spacecraft moving in a circular Keplerian orbit in the geomagnetic field. The method is developed based on the electrodynamics effect of the ...

        Attitude stabilization of a rigid spacecraft in the geomagnetic field 

        Natl Res Inst Astron & Geophys Helwan; Universidade Estadual Paulista (Unesp) (Elsevier B.V., 2007-01-01)
        An analytical method is proposed to study the attitude stability of a triaxial spacecraft moving in a circular Keplerian orbit in the geomagnetic field. The method is developed based on the electrodynamics effect of the ...

        Planar powered Swing-By maneuvers to brake a spacecraft 

        Inst Nacl Pesquisas Espaciais; Universidade Estadual Paulista (Unesp) (Springer, 2018-12-01)
        The Swing-By maneuver is a technique used in many space mission to modify the trajectory of a spacecraft. The most usual goal is to increase the energy of the spacecraft, but it is also possible to reduce this energy. An ...

        Attitude stabilization of a rigid spacecraft in the geomagnetic field 

        Abdel-Aziz, Yehia A. (Elsevier B.V., 2014)

        Tethered slingshot maneuver in the three-dimensional space 

        Universidade Estadual Paulista (Unesp); INPE (2018-01-01)
        The Tethered Slingshot maneuver (TSSM) is an alternative solution to maneuver a spacecraft in space, which is based in the use of cables. A space tether usually consists in two fixed objects at the end of a cable. In this ...

        TRAJECTORY ANALYSIS OF A SPACECRAFT MAKING A THREE-DIMENSIONAL POWERED SWING-BY MANEUVER 

        Universidade Estadual Paulista (Unesp); INPE (Univelt Inc, 2019-01-01)
        The present paper studies the problem of orbital maneuvers performed combining the passage of a spacecraft by a celestial body with an impulse applied to the spacecraft during the close approach. The motion of the spacecraft ...
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        Red de Repositorios Latinoamericanos
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        Dirección de Servicios de Información y Bibliotecas (SISIB)
        Universidad de Chile
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        Dirección de Servicios de Información y Bibliotecas (SISIB)
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