Matlab code for the determination of the reentry trajectory, deceleration profiles, and heat flux of the ARD capsule during orbital reentry into Earth's atmosphere.
The cases differ based on a fixed flight path angle 'gamma' or a fixed ballistic coefficient 'B'.
Comparison between analytical and numerical methods.
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Matlab code for the determination of the reentry trajectory, deceleration profiles, and heat flux of the ARD capsule during orbital reentry into Earth's atmosphere.
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Lfariello/Atmospheric_reentry
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Matlab code for the determination of the reentry trajectory, deceleration profiles, and heat flux of the ARD capsule during orbital reentry into Earth's atmosphere.
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