U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Control system having variably biased manipulatable unit

Patent 4580210 Issued on April 1, 1986. Estimated Expiration Date: Icon_subject April 17, 2004. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

Helicopter stick force augmentation null offset compensation
Patent #: 4078749
Issued on: 03/14/1978
Inventor: Johnson, Jr.

Fail safe force feel system
Patent #: 4106728
Issued on: 08/15/1978
Inventor: Griffith

Steering mechanism with an active force feedback, especially for aircraft
Patent #: 4236685
Issued on: 12/02/1980
Inventor: Kissel

Force feel actuator fault detection with directional threshold
Patent #: 4294162
Issued on: 10/13/1981
Inventor: Fowler ,   et al.

Force feel actuator with limited proportional/integral error feedback
Patent #: 4313165
Issued on: 01/26/1982
Inventor: Clelford ,   et al.

Helicopter force feel actuator automatic static null compensation
Patent #: 4382281
Issued on: 05/03/1983
Inventor: Fowler ,   et al.

Dual inner loop fault inhibit of aircraft outer loop
Patent #: 4417308
Issued on: 11/22/1983
Inventor: Wright ,   et al.

Biodynamic resistant control stick
Patent #: 4477043
Issued on: 10/16/1984
Inventor: Repperger

Automatic flight control pilot assist system Patent #: 4527242
Issued on: 07/02/1985
Inventor: McElreath ,   et al.

Inventor

Assignee

Application

No. 06/601260 filed on 04/17/1984

US 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 vehicle

Examiners

Primary: Smith, Jerry
Assistant: Grossman, Jon D.

Attorney, Agent or Firm

International Class

G05D 1/00 (20060101)

Foreign Application Priority Data

1983-04-18 SE

Abstract

In 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.

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