Equations of motion for the two-axes yaw-pitch gimbal configuration are dis
cussed on the assumption that the gimbals are rigid bodies and have no mass
unbalance. The equations are derived and different terms are brought toget
her into separate groups for the sake of clarity and to facilitate certain
interpretations. Different kinds of disturbances and their elimination or r
eduction are discussed, as is the yaw gain dependence on the pitch angle. I
nertia cross couplings are also given. The purpose is twofold: to simplify
the picture of the two-axes gimbals and to further illustrate the propertie
s of this configuration.