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Analysis Code for High Altitude Balloons - FedOA - Università degli ...

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ACHAB: <strong>Analysis</strong> <strong>Code</strong> <strong>for</strong> <strong>High</strong> <strong>Altitude</strong> <strong>Balloons</strong> Chapter 3<br />

The Mean Anomaly (MA) can be determined as follows:<br />

MA<br />

= 2π<br />

Day<br />

number<br />

DaysPerYear<br />

where DaysPerYear is the total number of days in a year <strong>for</strong> the considered planet<br />

(<strong>for</strong> Earth = 365) and Day number is the number of the balloon flight day starting from<br />

perihelion (<strong>for</strong> Earth, perihelion occurs on January 2).<br />

The true anomaly (TA) can be approximated by the following equation provided that<br />

the orbital eccentricity is small:<br />

5<br />

TA ≈ MA + 2esin<br />

2<br />

4<br />

2 ( MA)<br />

+ e sin(<br />

MA)<br />

The solar irradiance flux at the top of the atmosphere is related to the position of the<br />

planet (Earth) along its orbit around the Sun:<br />

I<br />

1367.<br />

5 ⎡1+<br />

ecos<br />

=<br />

( ) 2<br />

TA<br />

Sun 2<br />

2<br />

R ⎢<br />

⎣ 1−<br />

e ⎥ [W/m<br />

AU<br />

⎦<br />

2 ]<br />

For Earth: R = 1 and e = 0.<br />

016708.<br />

The constant 1367.5 [W/m 2 ] is the nominal<br />

AU<br />

value of the solar constant 32 .<br />

At the balloon altitude Z, the direct solar irradiance is equal to the product of its<br />

value at the top of the atmosphere and the atmospheric transmittance:<br />

I = I τ<br />

SunZ<br />

Thus the direct solar flux acting on the balloon is:<br />

Sun<br />

SunZ<br />

Sun<br />

⎤<br />

atm<br />

q = I [W/m 2 ]<br />

35

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