Patents Assigned to UNIBASE INFORMATION CORP.
  • Patent number: 9459119
    Abstract: An aircraft guidance system includes a reviewing and video synchronization device connected to a display panel. The display panel receives and displays guidance status of an aircraft. The reviewing and video synchronization device includes an operator panel, a video recording unit and a built-in recording unit. The operator panel includes a display screen and a plurality of keys. The display screen and the display panel synchronizedly display information. The video recording unit records the information displayed on the display screen. The built-in recording unit records the scanning signals and time stamps received by the display panel.
    Type: Grant
    Filed: March 12, 2015
    Date of Patent: October 4, 2016
    Assignee: Unibase Information Corp.
    Inventor: Cheng-Hsiang Lin
  • Patent number: 9177483
    Abstract: A guiding method for aircraft docking process, which is used to detect an aircraft when docking to a stop line along a J-line on apron, includes steps as followed. According to response distances of different positions from a laser scanner, a distance between the aircraft and the stop line and offset angle during the docking process are detected. To show the distance and offset angle on a data display panel as guiding reference when a pilot of the aircraft operates the aircraft. The guiding method further has a waiting stage, a positioning stage, and a distinguishing stage and a guiding stage.
    Type: Grant
    Filed: November 20, 2013
    Date of Patent: November 3, 2015
    Assignee: Unibase Information Corp.
    Inventor: Cheng-Hsiang Lin
  • Publication number: 20150142218
    Abstract: A guiding method for aircraft docking process, which is used to detect an aircraft when docking to a stop line along a J-line on apron, includes steps as followed. According to response distances of different positions from a laser scanner, a distance between the aircraft and the stop line and offset angle during the docking process are detected. To show the distance and offset angle on a data display panel as guiding reference when a pilot of the aircraft operates the aircraft. The guiding method further has a waiting stage, a positioning stage, and a distinguishing stage and a guiding stage.
    Type: Application
    Filed: November 20, 2013
    Publication date: May 21, 2015
    Applicant: UNIBASE INFORMATION CORP.
    Inventor: CHENG-HSIANG LIN