Patents Examined by Saul M. Bergman
  • Patent number: 4992713
    Abstract: An autopilot with long term yaw coordination capabilities which utilizes lateral acceleration to generate a rudder force command which is combined with the sensed rudder force to create an error signal which is combined with a rudder servo velocity signal and then integrated to create a virtual rudder position feedback signal for combination with the rudder position commands, generated from yaw rate information.
    Type: Grant
    Filed: October 11, 1988
    Date of Patent: February 12, 1991
    Assignee: Rockwell International Corporation
    Inventors: James H. McCollum, Gary E. Forquer
  • Patent number: 4689541
    Abstract: A method and apparatus are provided for simultaneously controlling a plurality of stepper motors. Addressing circuitry generates address data for each motor in a periodic address sequence. Memory circuits respond to the address data for each motor by accessing a corresponding memory location containing a first operational data set functionally related to a direction for moving the motor, speed data, and rate of speed change. First logic circuits respond to the first data set to generate a motor step command. Second logic circuits respond to the command from the first logic circuits to generate a third data set for replacing the first data set in memory with a current operational motor status, which becomes the first data set when the motor is next addressed.
    Type: Grant
    Filed: July 22, 1986
    Date of Patent: August 25, 1987
    Assignee: The United States of America as represented by the United States Department of Energy
    Inventors: Rollin G. Jones, Bert L. Kortegaard, David F. Jones
  • Patent number: 4583030
    Abstract: Aircraft attitude along the pitch axis is controlled by inputting a velocity command to a pitch control subsystem that includes a velocity side channel and a gain side channel of a pitch servo amplifier. An output from each channel of the pitch servo amplifier is applied to a pitch servo motor for positioning a primary control surface. The velocity of the pitch servo motor is detected by a velocity detector that generates a velocity feedback signal and control signals for each channel of the pitch servo amplifier. Also responsive to the velocity signal of the detector is a pre-flight test circuit for pre-flight checkout of the pitch control subsystem. In each line from the output of the channels of the pitch servo amplifier is a current detector that is part of a pitch trim control subsystem that responds to the current through the pitch servo motor to generate a trim velocity command signal. This velocity command signal is input to a velocity side channel and a gain side channel of a trim servo amplifier.
    Type: Grant
    Filed: August 3, 1982
    Date of Patent: April 15, 1986
    Assignee: Century Flight Systems, Inc.
    Inventor: John M. Nixon
  • Patent number: 4567418
    Abstract: In a control apparatus controlling point-to-point movement of arms of a robot, stepping motors are used to drive the shafts of the robot arms respectively, and motor drivers drive the stepping motors according to a 1-2-phase excitation mode in a low speed range but according to a 2-phase excitation mode in an intermediate and a high speed range.
    Type: Grant
    Filed: August 15, 1984
    Date of Patent: January 28, 1986
    Assignee: Hitachi, Ltd.
    Inventors: Akinobu Takemoto, Kenzo Takeichi, Yuhiko Yabe, Yoshiaki Yoshikawa
  • Patent number: 4414631
    Abstract: The discharge of a capacitor energizes a relay to actuate the dump valve of a braking system to interrupt braking action upon the occurrence of wheel slide.
    Type: Grant
    Filed: April 22, 1981
    Date of Patent: November 8, 1983
    Assignee: The Garrett Corporation
    Inventor: Arden L. Schug