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
Inducement of organogenetic tolerance for pancreatic xenotransplant
Imaging apparatus having selection unit to select focus detection areas
Method and apparatus for feeding a polyurethane mixture into hollow bodies
Method of manufacturing toner
System for encrypting and decrypting a plaintext message with authentication
Apparatus and method for evaluating an activity distribution, and irradiation system
Split-ring resonator creating a photonic metamaterial
  Randomly Featured Patents
Combustion vibration estimating apparatus, plant and gas turbine plant
X-Ray lithographic system
Water level alarm apparatus
Structure for supporting resistance cylinders
Keeper for a locking container door
Method and system for assisting a user to engage in a microbrowser-based interactive chat session
Bucket extractor device
High affinity immunoglobulin E receptor-like protein
Digital repetition rate check circuit
Sleeve for coupling a refrigerant pipe to a compressor container