for following parameters calculate, compare and discuss the $4$ worst case disturbance torques on earth and mars orbits.

a$.$ earth orbit $550$ km circular, mars orbit $250$ km circular

b$.$ spacecraft size cubic X$*$Y$*$Z$=1\mathrm{.}5*1\mathrm{.}5*2$ m$3,$ area to sun is X$*$Z$,$ area to direction of motion is X$*$Y$,$

c$.$ max derivation of the Z axis is $3$ degrees,

d$.$ Iz$=90$kg$/$m$2,$ Iy$=65$kg$/$m$2,$ Ix$=60$kg$/$m$2$

e$.$ location of center of solar pressure from lander center of gravity $0\mathrm{.}35$ m$,$

f$.$ location of center of aerodynamic pressure from lander center of gravity $0\mathrm{.}25$m$,$

g$.$ reflectance factor of $0\mathrm{.}65,$

h$.$ angle of incidence of the sun of $5$ degrees,

i$.$ lander magnetic dipole of $2$A$.$m$2$