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bateramos / GeneticLander

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Implement air drag in the simulation #8

Open bateramos opened 7 years ago

bateramos commented 7 years ago

D = Cd .5 r V^2 A Drag = Constant 0.5 Density velocity^2 Reference area https://www.grc.nasa.gov/WWW/K-12/airplane/falling.html https://www.grc.nasa.gov/WWW/K-12/airplane/drageq.html

bateramos commented 7 years ago

https://en.wikipedia.org/wiki/Apollo_Command/Service_Module#Command_Module_.28CM.29

bateramos commented 6 years ago

before implementing this, we should transform the simulation in a Newtonian one.