For many space applications, such as
communication, weather, military, and scientific
experiment satellites scanning precise regions, it
is necessary to maintain a satellite in a fixed
orientation relative to the earth. Unfortunately,
a correctly positioned satellite deviates with
time from this preferred orientation due to
perturbing environmental forces. This explains
considerable interest in libra-tional stability
study in recent times.
Among the numerous methods developed for
librational control, a passive technique depending
on the gradient of the gravitational field has
gained attention. Depending on the orbital
distance, environmental effects, such as,
aerodynamic, radiation, and magnetic torques,
become significant compared to the
gravity-gradient restoring moment. A need to
determine the influence of these disturbing forces
is thus evident.