Revisions to be included in 'Space Shuttle Guidance, Navigation and Control Design Equations' are reported. Technical changes include: (1) a plane change maneuver was incorporated in the program's logic; (2) in the search for an apsidal crossing, program checks were included to update through intervals of pi in the case of near circular orbits or close proximity to an apsidal point; (3) following an astronaut overwrite of a Lambert maneuver, the state vector was updated to establish a new target vector for use in the powered flight routine; and (4) following the computation of each maneuver, the position vector of the primary vehicle was offset - to help compensate for the effects of the finite maneuver - prior to the update of the state vector to the next maneuver point. Input and output variables, detailed flow diagrams a functional flow diagram, and a description of equations are presented.


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    Titel :

    Rendezvous targeting


    Beteiligte:

    Erscheinungsdatum :

    1973-07-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Rendezvous targeting for space missions

    Tempelman, W. H. | NTRS | 1972


    On-Board Rendezvous Targeting for Orion

    M. W. Weeks / C. N. DSouza | NTIS | 2010


    Trigger Angle Targeting for Orbital Rendezvous

    Woffinden, David C. / Ben Rose, M. / Geller, David K. | Online Contents | 2008


    Trigger Angle Targeting for Orbital Rendezvous

    Woffinden, David C | Online Contents | 2008


    Trigger Angle Targeting for Orbital Rendezvous

    Woffinden, David C. / Rose, M. / Geller, David K. | Springer Verlag | 2008