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| File Information |
| Description |
This program is a model 3 points.
Take 3 inputs:
1° --> altitude [m]
2° --> weight [Kg]
3° --> time [s]
The output combinations are 12:
1° --> altitude / time [m/s]
2° --> time / altitude [s/m]
3° --> altitude / weight [m/Kg]
4° --> weight / altitude [Kg/m]
5° --> weight / time [Kg/s]
6° --> time / weight [s/Kg]
7° --> altitude * weight / time [m*Kg/s]
8° --> altitude / ( time * weight ) [m/(s*Kg)]
9° --> time * weight / altitude [s*Kg/m]
10° --> time / ( weight * altitude ) [s/(Kg*m)]
11° --> altitude * time / weight [m*s/Kg]
12° --> weight / ( time * altitude ) [Kg/(s*m)]
The tridimensional reference system is XZT where:
X --> horizontal dimension of the plane (monitor width)
Z --> vertical dimension of the plane (monitor altitude)
T --> profundity (the third dimension)
The altitude variable is the length (for example a car on the street) in the XZ plane and also it is the length (for example the water from the sky) in the T line of third dimension.
A man is running 100 meters in 10 seconds with weight 70 Kg.
to insert a positive number of altitude [m]: 100
to insert a positive number of weight [Kg]: 70
to insert a positive number of time [s]: 10
The outputs are:
altitude / time [m/s] 10
time / altitude [s/m] 0.1000
altitude / weight [m/Kg] 1.4286
weight / altitude [Kg/m] 0.7000
weight / time [Kg/s] 7
time / weight [s/Kg] 0.1429
altitude * weight / time [m*Kg/s] 700
altitude / ( time * weight ) [m/(s*Kg)] 0.1429
time * weight / altitude [s*Kg/m] 7
time / ( weight * altitude ) [s/(Kg*m)] 0.0014
altitude * time / weight [m*s/Kg] 14.2857
weight / ( time * altitude ) [Kg/(s*m)] 0.0700
The 1° output is the velocity.
The 8° output is the acceleration.
The 10° output is the force. |
| MATLAB release |
MATLAB 6.1 (R12.1)
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| Zip File Content |
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| Other Files |
license.txt, MOV.m
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| Updates |
| 21 Feb 2009 |
Add of Database4 and Database6, double physics ACCESS model. |
| 09 Aug 2009 |
grammar review, generic review |
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