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Home / Scripts / Scientific/Engineering / Astronomy/Aerospace

SSTSLAB




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Category:
Yi Chen | More scripts
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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