Patents by Inventor Sunil Kumar KS

Sunil Kumar KS 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).

  • System and method for monitoring compliance with air traffic control instructions
    Patent number: 10755583
    Abstract: A method is provided for monitoring compliance with air traffic control (ATC) instructions by an air crew of an aircraft. First, voice and text ATC commands are received by an ATC instruction moderator support system (AIMSS) located on board the aircraft. The voice and text ATC commands are converted into a data format by the AIMSS. The ATC commands are used to determine an expected aircraft state while a current aircraft state is determined by the aircraft sensors. The current aircraft state is compared with the expected state and determined if it is in compliance. If the current state is in non-compliance, it is determined if the non-compliance is allowable and it is then classified as either no action or incorrect action by the aircrew. Finally, an alert of the noncompliance is generated with the AIMSS.
    Type: Grant
    Filed: October 23, 2017
    Date of Patent: August 25, 2020
    Assignee: HONEYWELL INTERNATIONAL INC.
    Inventors: Abneesh Singla, Sreenivasan Govindillam K, Srinivas D. Gonabal, Pradeep Huncha, Vedavyas Rallabandi, Jaibir Singh, Sunil Kumar KS
  • SYSTEM AND METHOD FOR MONITORING COMPLIANCE WITH AIR TRAFFIC CONTROL INSTRUCTIONS
    Publication number: 20190122564
    Abstract: A method is provided for monitoring compliance with air traffic control (ATC) instructions by an air crew of an aircraft. First, voice and text ATC commands are received by an ATC instruction moderator support system (AIMSS) located on board the aircraft. The voice and text ATC commands are converted into a data format by the AIMSS. The ATC commands are used to determine an expected aircraft state while a current aircraft state is determined by the aircraft sensors. The current aircraft state is compared with the expected state and determined if it is in compliance. If the current state is in non-compliance, it is determined if the non-compliance is allowable and it is then classified as either no action or incorrect action by the aircrew. Finally, an alert of the noncompliance is generated with the AIMSS.
    Type: Application
    Filed: October 23, 2017
    Publication date: April 25, 2019
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Abneesh Singla, Sreenivasan Govindillam K, Srinivas D. Gonabal, Pradeep Huncha, Vedavyas Rallabandi, Jaibir Singh, Sunil Kumar KS