Consider an axi-symmetric dual spin stabilized spacecraft with ISR = 20 nm s−2 and IT = 30 nm s−2 and 𝜔R = 100 rpm, ISP = 25 nm s−2 and 𝜔P = 1 rpm. Find the nutation frequency 𝜔n in rad s−1 and...

Consider an axi-symmetric dual spin stabilized spacecraft with ISR = 20 nm s−2 and IT = 30 nm s−2 and 𝜔R = 100 rpm, ISP = 25 nm s−2 and 𝜔P = 1 rpm. Find the nutation frequency 𝜔n in rad s−1 and determine the conditions for stability of this satellite.