%%Función que calcula el potencial gravitatorio de un asteroide elipsoidal %%dada su geometría y su densidad function [GGU U]=GGpot(x,y,z,GEO,mu) %%%GEO=[a b c]% %%%mu=constante gravitacional (volumen*densidad*G) a=GEO(1);b=GEO(2);c=GEO(3); Rm=(a+b+c)/2; ti=[a-b;b-c]; A=[(b/2*(Rm/a)^2-a/2*(Rm/b)^2) -(3*b*(Rm/a)^2+3*a*(Rm/b)^2);(c/2*(Rm/b)^2+b*(Rm/c)^2) (3*c*(Rm/b)^2)]; Cost=A\ti; J2=Cost(1); J22=Cost(2); r=sqrt(x^2+y^2+z^2); phi=asin(z/r); if y>=0 lambda=acos(x/r/cos(phi)); else lambda=2*pi-acos(x/r/cos(phi)); end U=mu/r*(1+J2/2*(Rm/r)^2*(1-3*sin(phi)^2)-3*J22*(Rm/r)^2*cos(phi)^2*cos(2*lambda)); Ur=-r^-1*(U)+mu/r*(-J2*(Rm^2/r^3)*(1-3*sin(phi)^2)+6*J22*(Rm^2/r^3)*cos(phi)^2*cos(2*lambda)); Ul=mu/r*(6*J22*(Rm/r)^2*cos(phi)^2*sin(2*lambda)); Up=mu/r*(-J2*(Rm/r)^2*3*sin(phi)*cos(phi)+6*J22*(Rm/r)^2*cos(phi)*sin(phi)*cos(2*lambda)); B=[cos(phi)*cos(lambda) cos(phi)*sin(lambda) sin(phi);-r*cos(phi)*sin(lambda) r*cos(phi)*cos(lambda) 0;-r*sin(phi)*cos(lambda) -r*sin(phi)*sin(lambda) r*cos(phi)]; GU=B\[Ur Ul Up]'; % er=[cos(phi)*cos(lambda) cos(phi)*sin(lambda) sin(phi)]'; % ep=[-sin(phi)*cos(lambda) -sin(phi)*sin(lambda) cos(phi)]'; % el=[-cos(phi)*sin(lambda) cos(phi)*cos(lambda) 0]'; % % GU=Ur*er+1/r*Up*ep+1/r*cos(phi)*Ul*el; %Uxx inc=1e-10; x=x+inc; r=sqrt(x^2+y^2+z^2); phi=asin(z/r); if y>=0 lambda=acos(x/r/cos(phi)); else lambda=2*pi-acos(x/r/cos(phi)); end U=mu/r*(1+J2/2*(Rm/r)^2*(1-3*sin(phi)^2)-3*J22*(Rm/r)^2*cos(phi)^2*cos(2*lambda)); Ur=-r^-1*(U)+mu/r*(-J2*(Rm^2/r^3)*(1-3*sin(phi)^2)+6*J22*(Rm^2/r^3)*cos(phi)^2*cos(2*lambda)); Ul=mu/r*(6*J22*(Rm/r)^2*cos(phi)^2*sin(2*lambda)); Up=mu/r*(-J2*(Rm/r)^2*3*sin(phi)*cos(phi)+6*J22*(Rm/r)^2*cos(phi)*sin(phi)*cos(2*lambda)); B=[cos(phi)*cos(lambda) cos(phi)*sin(lambda) sin(phi);-r*cos(phi)*sin(lambda) r*cos(phi)*cos(lambda) 0;-r*sin(phi)*cos(lambda) -r*sin(phi)*sin(lambda) r*cos(phi)]; GUinc=B\[Ur Ul Up]'; GGU(1)=(GUinc(1)-GU(1))/inc; %Uyy y=y+inc; r=sqrt(x^2+y^2+z^2); phi=asin(z/r); if y>=0 lambda=acos(x/r/cos(phi)); else lambda=2*pi-acos(x/r/cos(phi)); end U=mu/r*(1+J2/2*(Rm/r)^2*(1-3*sin(phi)^2)-3*J22*(Rm/r)^2*cos(phi)^2*cos(2*lambda)); Ur=-r^-1*(U)+mu/r*(-J2*(Rm^2/r^3)*(1-3*sin(phi)^2)+6*J22*(Rm^2/r^3)*cos(phi)^2*cos(2*lambda)); Ul=mu/r*(6*J22*(Rm/r)^2*cos(phi)^2*sin(2*lambda)); Up=mu/r*(-J2*(Rm/r)^2*3*sin(phi)*cos(phi)+6*J22*(Rm/r)^2*cos(phi)*sin(phi)*cos(2*lambda)); B=[cos(phi)*cos(lambda) cos(phi)*sin(lambda) sin(phi);-r*cos(phi)*sin(lambda) r*cos(phi)*cos(lambda) 0;-r*sin(phi)*cos(lambda) -r*sin(phi)*sin(lambda) r*cos(phi)]; GUinc=B\[Ur Ul Up]'; GGU(2)=(GUinc(2)-GU(2))/inc; %Uzz z=z+inc; r=sqrt(x^2+y^2+z^2); phi=asin(z/r); if y>=0 lambda=acos(x/r/cos(phi)); else lambda=2*pi-acos(x/r/cos(phi)); end U=mu/r*(1+J2/2*(Rm/r)^2*(1-3*sin(phi)^2)-3*J22*(Rm/r)^2*cos(phi)^2*cos(2*lambda)); Ur=-r^-1*(U)+mu/r*(-J2*(Rm^2/r^3)*(1-3*sin(phi)^2)+6*J22*(Rm^2/r^3)*cos(phi)^2*cos(2*lambda)); Ul=mu/r*(6*J22*(Rm/r)^2*cos(phi)^2*sin(2*lambda)); Up=mu/r*(-J2*(Rm/r)^2*3*sin(phi)*cos(phi)+6*J22*(Rm/r)^2*cos(phi)*sin(phi)*cos(2*lambda)); B=[cos(phi)*cos(lambda) cos(phi)*sin(lambda) sin(phi);-r*cos(phi)*sin(lambda) r*cos(phi)*cos(lambda) 0;-r*sin(phi)*cos(lambda) -r*sin(phi)*sin(lambda) r*cos(phi)]; GUinc=B\[Ur Ul Up]'; GGU(3)=(GUinc(3)-GU(3))/inc; e-REdING. Biblioteca de la Escuela Superior de Ingenieros de Sevilla.


DISEÑO DE MISIONES DE RENDEZVOUS CON ASTEROIDES PRÓXIMOS A LA TIERRA

: Montilla García, José Manuel
: Grado en Ingeniería Aeroespacial
Contenido del proyecto: