An aircraft landing wheel assembly comprising a set of rotating components
and a set of static components wherein an applied electrical current
applied to conductive elements associated with one set of components
gives rise to primary magnetic fields which interact with reactive
magnetic fields associated with the other set of components whereby the
interaction of magnetic field forces gives rise to rotational forces
which act on the rotating components of said aircraft landing wheel
assembly to induce controlled forward rotation of the landing wheel prior
to contact with the runway and controlled retardation assistance as
required during deceleration of the aircraft after touch down with the
runway.