Patent ReferencesHelicopter stick force augmentation null offset compensation Fail safe force feel system Steering mechanism with an active force feedback, especially for aircraft Force feel actuator fault detection with directional threshold Force feel actuator with limited proportional/integral error feedback Helicopter force feel actuator automatic static null compensation Dual inner loop fault inhibit of aircraft outer loop Biodynamic resistant control stick Automatic flight control pilot assist system Patent #: 4527242 InventorAssigneeApplicationNo. 06/601260 filed on 04/17/1984US Classes:700/85, Positional (e.g., joystick)244/17.13, Automatic or condition responsive control244/223, With feel244/227, With electric control244/230, With variable output318/580, Vehicular guidance systems with single axis control318/628, "Feelback" systems701/3Aeronautical vehicleExaminersPrimary: Smith, JerryAssistant: Grossman, Jon D. Attorney, Agent or FirmInternational ClassG05D 1/00 (20060101)Foreign Application Priority Data1983-04-18 SEAbstractIn a control system having a manipulatable unit, such as an aircraft stick, which is biased toward a neutral position to provide control "feel", an input which at each instant signifies the position of displacement of the stick from its neutral position is processed to provide an output signifying the magnitude of the biasing force to be applied to the stick. In a range of positions spaced to one side of its neutral position (or in such a range at each side of neutral) the output provides for a steep biasing force gradient as the stick is moved through a predetermined distance in either direction from a turning point to which the stick had been brought by movement in the opposite direction. For all other movements of the stick within that range the biasing force has a low gradient. The higher gradient of bias for small trimming movements provides better feel for trimming without requiring stick bias to be unduly stiff during coarser stick displacements. | |