1. 0 1 - 0 tosc/lU
2. {-O.S/toraXO]l|v£C£rtOIIv£CEF(0SCD} (5) where f&ECEfit)] gives the air density as a function of altitude from the 1976 U.S. Standard Atmosphere19, S is the spacecraft's aerodynamic reference area, and CD is its drag coefficient. Other disturbances, such as solar radiation pressure and outgassing, have not been modeled becausethe two torques ineq. (4) are often the dominant attitudedisturbances in low Earth orbit.
3. 0 0 0 0 -4co20a10 0 0 0