1. An aircraft steering system comprising:
a steerable nose-landing gear, and
to receive a steering input representative of a desired direction of travel of the steerable nose landing gear, and
to receive one or more force-based inputs representative of lateral forces acting upon the nose landing gear,
wherein the lateral forces are forces with a component in a lateral direction perpendicular to a longitudinal axis and a vertical
axis of the aircraft, and
wherein the controller is adapted to automatically adjust the steering input based upon the one or more force-based inputs
and output an adjusted steering command for a steering actuator of the nose landing gear.