Package com.titan.controls

Class Wind

java.lang.Object

com.titan.controls.Wind

public class Wind
extends Object

Nested Class Summary

Nested Classes

Modifier and Type	Class	Description
static enum	Wind.WindType

Constructor Summary

Constructors

Constructor	Description
Wind(Wind.WindType windType)

Method Summary

Modifier and Type	Method	Description
void	blow(LandingModule module, double stepSize, double currentTime)
static double	calculateAirDensity(double altitude)
static double	calculatePressure(double altitude)	Matlab polyfit for the coefficients - data from NASA (https://attic.gsfc.nasa.gov/huygensgcms/Titan_atmos.gif) Matlab function: f5 = @(x) -0.000000000079339.
static double	calculateTemperature(double altitude)	Matlab polyfit for the coefficients - data from NASA (https://attic.gsfc.nasa.gov/huygensgcms/Titan_atmos.gif) Matlab function: f6 = @(x) -0.000000000282784.
double	getWindAngle()
double	getWindSpeed()

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Constructor Details

Wind

public Wind(Wind.WindType windType)

Method Details

getWindSpeed

public double getWindSpeed()

getWindAngle

public double getWindAngle()

blow

public void blow(LandingModule module,
 double stepSize,
 double currentTime)

calculateAirDensity

public static double calculateAirDensity(double altitude)

calculateTemperature

public static double calculateTemperature(double altitude)

Matlab polyfit for the coefficients - data from NASA (https://attic.gsfc.nasa.gov/huygensgcms/Titan_atmos.gif)
Matlab function: f6 = @(x) -0.000000000282784.*x.^6 + 0.000000160592161.*x.^5 -0.000033550883549.*x.^4 + 0.003020265171911.*x.^3 -0.095206120316128.*x.^2 + 0.219198689819765.*x + 88.631154566255688

Parameters:

altitude -

Returns:

calculatePressure

public static double calculatePressure(double altitude)

Matlab polyfit for the coefficients - data from NASA (https://attic.gsfc.nasa.gov/huygensgcms/Titan_atmos.gif)
Matlab function: f5 = @(x) -0.000000000079339.*x.^5 + 0.000000049373809.*x.^4 - 0.000011714823097.*x.^3 + 0.001320377017440.*x.^2 - 0.071004201806174.*x + 1.494389829591593

Parameters:

altitude -

Returns: