Aircraft flight management unit and method of monitoring such a unit

    公开(公告)号:US09922568B2

    公开(公告)日:2018-03-20

    申请号:US15351852

    申请日:2016-11-15

    IPC分类号: G05D1/02 G08G5/00 G05D1/10

    摘要: A flight management unit includes two guidance subsystems each including a flight management system, each of the flight management systems being configured at least to extract a flight plan from at least one navigation database, to construct a flight trajectory, and to compute guidance commands for the aircraft. The flight management unit also includes at least one monitoring unit configured to compute a guidance command from a validated flight trajectory and a consolidated flight plan and to monitor the guidance command, as well as guidance commands computed by the two flight management systems so as to be able to detect and to identify a defective flight management system.

    Common operating environment for aircraft operations with air-to-air communication

    公开(公告)号:US09916764B2

    公开(公告)日:2018-03-13

    申请号:US15614042

    申请日:2017-06-05

    申请人: WxOps, Inc.

    IPC分类号: G08G5/00 G01C23/00 H04L29/08

    摘要: A common operating environment (COE) display system for vehicle operations, such as for air transport provides coordination of logistics information with dispatch or a controller. An operational plan, such as a flight plan or other operational plan describing vehicle deployment is stored, and a map visualization system displays a map region. An in-vehicle display depicts the operational plan, providing displays of current and projected operational conditions of the vehicle within different time phases of the operational plan. Communication as either text or other data allows transmission can be performed as text, attachments or a combination of text and attachments. Messages (text) and attachments (files) are exchanged only through the server, and the items exchanged are recorded for analysis and forensic purposes.

    METHOD FOR AUTOMATICALLY REJOINING A REFERENCE VERTICAL PROFILE OF AN AIRCRAFT

    公开(公告)号:US20170323573A1

    公开(公告)日:2017-11-09

    申请号:US15492693

    申请日:2017-04-20

    申请人: THALES

    IPC分类号: G08G5/00 B64D31/02

    摘要: A method, computer program and system are provided for calculating in an automatic manner a trajectory for rejoining a reference vertical profile of an aircraft. A reference vertical profile comprises a set of vertical constraints, and a method comprises a step of selecting an altitude constraint to be complied with, a step of calculating a vertical-profile prediction making it possible to comply with the constraint, a step of validating the vertical-profile prediction, if the vertical-profile prediction is validated, a step of applying the vertical-profile prediction, otherwise a step of determining the existence of a following altitude constraint to be complied with; if a following altitude constraint exists: a step of selecting a following altitude constraint to be complied with; a return to the step of detecting non-compliance with an altitude constraint; otherwise, a step of applying an exit procedure.