Patents by Inventor Mahanth Gowda

Mahanth Gowda has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 10960285
    Abstract: Systems and techniques for sensor-derived object flight performance tracking are described herein. A set of magnetometer readings may be obtained from a magnetometer included with an object. A local rotation axis of the object may be determined at a time using the set of magnetometer readings. The local rotation axis may describe rotation of the object around a local magnetic target. A global rotation axis may be calculated based on an initial orientation of the object. The global rotation axis may describe a fixed rotation axis of the object during flight in a global coordinate frame, wherein an angle between the global rotation axis and magnetic north remains constant during the flight. An orientation of the object may be determined for the time using the global rotation axis and the local rotation axis of the object at the time.
    Type: Grant
    Filed: August 27, 2019
    Date of Patent: March 30, 2021
    Assignee: Intel Corporation
    Inventors: Narayan Sundararajan, Xue Yang, Suresh V. Golwalkar, Mahanth Gowda, Romit Roy Choudhury
  • Publication number: 20200009439
    Abstract: Systems and techniques for sensor-derived object flight performance tracking are described herein. A set of magnetometer readings may be obtained from a magnetometer included with an object. A local rotation axis of the object may be determined at a time using the set of magnetometer readings. The local rotation axis may describe rotation of the object around a local magnetic target. A global rotation axis may be calculated based on an initial orientation of the object. The global rotation axis may describe a fixed rotation axis of the object during flight in a global coordinate frame, wherein an angle between the global rotation axis and magnetic north remains constant during the flight. An orientation of the object may be determined for the time using the global rotation axis and the local rotation axis of the object at the time.
    Type: Application
    Filed: August 27, 2019
    Publication date: January 9, 2020
    Inventors: Narayan Sundararajan, Xue Yang, Suresh V. Golwalkar, Mahanth Gowda, Romit Roy Choudhury
  • Patent number: 10420999
    Abstract: Systems and techniques for sensor-derived object flight performance tracking are described herein. A set of magnetometer readings may be obtained from a magnetometer included with an object. A local rotation axis of the object may be determined at a time using the set of magnetometer readings. The local rotation axis may describe rotation of the object around a local magnetic target. A global rotation axis may be calculated based on an initial orientation of the object. The global rotation axis may describe a fixed rotation axis of the object during flight in a global coordinate frame, wherein an angle between the global rotation axis and magnetic north remains constant during the flight. An orientation of the object may be determined for the time using the global rotation axis and the local rotation axis of the object at the time.
    Type: Grant
    Filed: March 27, 2017
    Date of Patent: September 24, 2019
    Assignee: Intel Corporation
    Inventors: Narayan Sundararajan, Xue Yang, Suresh V. Golwalkar, Mahanth Gowda, Romit Roy Choudhury
  • Publication number: 20180272221
    Abstract: Systems and techniques for sensor-derived object flight performance tracking are described herein. A set of magnetometer readings may be obtained from a magnetometer included with an object. A local rotation axis of the object may be determined at a time using the set of magnetometer readings. The local rotation axis may describe rotation of the object around a local magnetic target. A global rotation axis may be calculated based on an initial orientation of the object. The global rotation axis may describe a fixed rotation axis of the object during flight in a global coordinate frame, wherein an angle between the global rotation axis and magnetic north remains constant during the flight. An orientation of the object may be determined for the time using the global rotation axis and the local rotation axis of the object at the time.
    Type: Application
    Filed: March 27, 2017
    Publication date: September 27, 2018
    Inventors: Narayan Sundararajan, Xue Yang, Suresh V. Golwalkar, Mahanth Gowda, Romit Roy Choudhury