matlab Apollo卫星的运动轨迹已知Apollo卫星的运动轨迹 满足下面的方程u0=1/82.43;u1=1-u0,r1=sqrt((x+u0)^2+y^2),r2=sqrt((x-u1)^2+y^2),DDx=2*Dy+x-u1*(x+u0)/r1^3-u0*(x-u1)/r2^3,DDy=-2*Dx+y-u0*y/r1^3-u1*y/r2^3,x(0)=1.2,Dx(0)=0,y(0)=0,D

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