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  • Home > Scripts > Scientific/Engineering > Astronomy/Aerospace

    SSTSLAB

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    Category:
    Yi Chen | More scripts
    www.mathworks.com
    Freeware 

    Windows / Linux / BSD / Solaris
    N/A
    Matlab
    July 31st, 2007, 14:10 GMT
    C: \ Scientific/Engineering \ Astronomy/Aerospace

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    SSTSLAB description

    SSTSLAB - Simple Space Tether Simulation Laboratory

    Simple Space Tether Simulation Laboratory (SSTSLAB) is a simulation tool for matlab/simulink, the current version is a beta version, it need more test work to make sure that the results are acceptable accurate.

    Set the SSTSLAB folder as the current work path of MATLAB, which includes the following

    files:
    No. File Name Description
    1 SSTS_Contents.m Contents for SSTSLAB
    2 SSTS__lib_math.mdl Some math blocks for tether simulation
    3 SSTS__tether_dumbbell.mdl Dumbbell tether simulation
    4 SSTS__tether_dumbbell_replot.m Plot figures for dumbbell tether
    5 SSTS__tether_MMET_I.mdl MMET-I tether simulation
    6 SSTS__tether_MMET_I_replot.m Plot figures for MMET-I
    7 SSTS__tether_MMET_II.mdl MMET-II tether simulation
    8 SSTS__tether_MMET_II_replot.m Plot figures for MMET-II
    9 SSTS__tether_MMET_II_discrete_number_case.mdl Discrete point mass case for MMET-II
    10 SSTS__tether_MMET_II_U_energy_plot.m Plot potential energy difference between concrete & discrete MMET-II model
    11 SSTS__tether_MMET_II_discrete_number_sfunction_I.m Discrete point masses s-function I for
    MMET-II
    12 SSTS__tether_MMET_II_discrete_number_sfunction_II.m Discrete point masses s-function II for
    MMET-II
    13 SSTS__tether_MMET_II_discrete_number_sfunction_III.m Discrete point masses s-function III for
    MMET-II
    14 SSTS__tether_MMET_II_discrete_number.m To calculate the location of each point mass within the tether for MMET-II
    15 SSTS__ln_function_singularity_plot.m To plot singularity for ln() function
    16 SSTS__clear.m To clear all data and figures in workspace
    17 SSTS__plot_orbit_position.m To plot the position function of orbits( cycles ) as follows:

    R(theta) =rp*(1 e)/(1 e*cos(theta))

    18 SSTS__plot_orbit_position3d.m To plot the position function of orbits( cycles ) as follows:
    R(theta) = rp*(1 e)/(1 e*cos(theta)) in 3D figure
    19 Jpg files To support mdl files



    TAGS:

    SSTSLAB script | matlab aerospace | SSTSLAB matlab | SSTSLAB | script | matlab

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