Resources Contact Us Home
Flight control system with tactile feedback

Image Number 3 for United States Patent #5062594.

A control system for an aircraft or other man-machine system wherein the usual visual feedback system is characterized and is optimally supplemented by a secondary feel oriented feedback arrangement in which input signals are derived from either of two supplementary feedback signal sources and the resulting algorithms characterized mathematically. The disclosure includes several exemplary arrangements of the feedback systems in which some of the input parameters are of selected value. Mathematical characterization of the feedback paths is used.

  Recently Added Patents
Bean variety RS 08071160
Data consolidation using a common portion accessible by multiple devices
System for presenting media programming guides
Augmented I/O for limited form factor user-interfaces
Wiring boards for array-based electronic devices
Method and apparatus for determining proper telephony adaptor configuration and installation
System and method for observing heart rate of passenger
  Randomly Featured Patents
Method and device for function selection of a control unit
System for rotatably mounting a vessel to a loading buoy
Inbred corn plant 22DHD11 and seeds thereof
Apparatus for extracting energy from winds at high altitudes
Fault tolerant automatic control system utilizing analytic redundancy
Mounting guard ring
Method for measuring network performance parity
Method for transmitting power control information for HS-SCCH in mobile communication system
On chip local MOSFET sizing