meca244.py

Created by acrozak02

Created on January 17, 2021

824 Bytes


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  force et champ de gravitation:
vect FA/B=-G*(mA*mB/r**2)vect uA-->B
vect FA/B=mB*vect&
G=6.67*10^-11N.m^2.kg^-2
vect&=-G*(mA/r**2)vect uA-->B

mouvement satellite et planetes:
referentielle astrocentrique considéré galiléen
muni du repere de Frenet centré sur P
vect FA/P=G*(m*M/r**2)(vect)u n 
soit vect FA/P=m*vect&
2)deuxieme loi de Newton appliquée
vect EF=m*(vect)a
G*(m*M/r**2)(vect)un=m*(vect)a
vect a=G*(M/r**2)vect un
-dans le repère de frenet centré sur P
vect a=v**2/r(vect)un+dv/dt(vect)ut
comme vect a=G*M/r**2 il vient:
-soit dv/dt=0
soit v=constante
-soit v**2/r=G*M/r**2
soit v=racine G*M/r
v=cst car M et r constantes

vect v=racine G*M/r (vect)ut
l application de la 2eme loi de newton
dans le repere frenet permet davoir les caracteristiques
du vect v et a.

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