System and Method for Rotorcraft Approach to Hover

    公开(公告)号:US20190039720A1

    公开(公告)日:2019-02-07

    申请号:US16030687

    申请日:2018-07-09

    Abstract: A rotorcraft having a power train, a rotor system coupled to the power train and comprising a plurality of rotor blades, a flight control system (FCS) operable to change at least one operating condition of the rotor system, a pilot control assembly (PCA) operable to receive commands from a pilot, and a flight control computer (FCC) in electrical communication between the FCS and the PCA. The FCC is operable to receive a pilot command to mark a target, designate a hover location in response to the pilot command to mark the target, receive a pilot command to return to the target, engage an approach-to-hover maneuver in response to the pilot command to return to the target, and transition, in response to engaging the approach-to-hover maneuver, to a second operating condition of the rotor system corresponding to a change in heading, a reduction in airspeed, and a descent in altitude.

    SYSTEM AND METHOD FOR ROTORCRAFT HEADING CONTROL

    公开(公告)号:US20180265190A1

    公开(公告)日:2018-09-20

    申请号:US15464084

    申请日:2017-03-20

    Abstract: In accordance with an embodiment of the present invention, a method of operating a rotorcraft includes operating the rotorcraft in a heading control mode that includes activating a yaw channel path of a heading controller and deactivating a roll channel path of the heading controller when a speed of the rotorcraft is less than a first speed threshold or a heading error is less than a heading error threshold, and activating the roll channel path of the heading controller and deactivating the yaw channel path of the heading controller when the speed of the rotorcraft is greater than a second speed threshold and the heading error is not less than the heading error threshold.

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