LANDING ZONE DESIGNATION SYSTEM AND METHOD

    公开(公告)号:US20210012672A1

    公开(公告)日:2021-01-14

    申请号:US17033164

    申请日:2020-09-25

    Inventor: John G. Williams

    Abstract: A landing zone designation system is provided that includes a master and a slave landing strobes. A detector on an aircraft can detect master and slave optical signals, and a processor can be coupled to the detector to compute placement of the aircraft relative to the master and slave landing strobes. A method is provided for designating a landing zone for an aircraft. The method includes emitting first and second optical signals, where a determination is made whether the aircraft is to land at a first landing zone or a second landing zone depending on a difference between the first optical signal and the second optical signal. A distance to landing within the determined first landing zone or the second landing zone can also be determined.

    Landing strobe signature
    2.
    发明授权

    公开(公告)号:US10815006B2

    公开(公告)日:2020-10-27

    申请号:US16371840

    申请日:2019-04-01

    Inventor: John G. Williams

    Abstract: A landing strobe is provided having an optical emitter configured to emit an optical signal. An input device can be coupled to the optical emitter for setting the optical signal to a signature strobe output unique to the landing strobe. A landing zone designation system is also provided having a landing strobe configured to emit a signature strobe output unique to the landing strobe. An aircraft spaced from the landing strobe can include a detector for optically receiving the signature strobe output to determine the landing zone is proper to land the aircraft if the signature strobe output matches an expected signature strobe output.

    LANDING STROBE, SYSTEM AND METHOD FOR DEPLOYING THE LANDING STROBE

    公开(公告)号:US20200307827A1

    公开(公告)日:2020-10-01

    申请号:US16371697

    申请日:2019-04-01

    Abstract: A landing strobe is provided that comprises a vane extending from the landing strobe, and an actuator coupled to the vane. The actuator can be configured to move the vane from a first position to a second position upon impact of the landing strobe. The landing strobe can also comprise an optical emitter configured to emit an adjustable radiation pattern extending radially around a central axis that is substantially vertical when the van is moved to the second position. A landing strobe system is also provided and comprises a landing strobe configured to be released from an aircraft arranged over a landing zone. The vane is configured to extend at an upward angle outward from the landing strobe when released from the aircraft. The vane is further configured to extend at a downward angle outward from the landing strobe when the landing strobe contacts the landing zone.

    LANDING ZONE DESIGNATION SYSTEM AND METHOD
    4.
    发明申请

    公开(公告)号:US20200312169A1

    公开(公告)日:2020-10-01

    申请号:US16371751

    申请日:2019-04-01

    Inventor: John G. Williams

    Abstract: A landing zone designation system is provided that includes a master and a slave landing strobes. A detector on an aircraft can detect master and slave optical signals, and a processor can be coupled to the detector to compute placement of the aircraft relative to the master and slave landing strobes. A method is provided for designating a landing zone for an aircraft. The method includes emitting first and second optical signals, where a determination is made whether the aircraft is to land at a first landing zone or a second landing zone depending on a difference between the first optical signal and the second optical signal. A distance to landing within the determined first landing zone or the second landing zone can also be determined.

    LANDING STROBE SIGNATURE
    5.
    发明申请

    公开(公告)号:US20200307828A1

    公开(公告)日:2020-10-01

    申请号:US16371840

    申请日:2019-04-01

    Inventor: John G. Williams

    Abstract: A landing strobe is provided having an optical emitter configured to emit an optical signal. An input device can be coupled to the optical emitter for setting the optical signal to a signature strobe output unique to the landing strobe. A landing zone designation system is also provided having a landing strobe configured to emit a signature strobe output unique to the landing strobe. An aircraft spaced from the landing strobe can include a detector for optically receiving the signature strobe output to determine the landing zone is proper to land the aircraft if the signature strobe output matches an expected signature strobe output.

    Landing strobe, system and method for deploying the landing strobe

    公开(公告)号:US10766638B1

    公开(公告)日:2020-09-08

    申请号:US16371697

    申请日:2019-04-01

    Abstract: A landing strobe is provided that comprises a vane extending from the landing strobe, and an actuator coupled to the vane. The actuator can be configured to move the vane from a first position to a second position upon impact of the landing strobe. The landing strobe can also comprise an optical emitter configured to emit an adjustable radiation pattern extending radially around a central axis that is substantially vertical when the van is moved to the second position. A landing strobe system is also provided and comprises a landing strobe configured to be released from an aircraft arranged over a landing zone. The vane is configured to extend at an upward angle outward from the landing strobe when released from the aircraft. The vane is further configured to extend at a downward angle outward from the landing strobe when the landing strobe contacts the landing zone.

    Landing zone designation system and method

    公开(公告)号:US11164470B2

    公开(公告)日:2021-11-02

    申请号:US17033164

    申请日:2020-09-25

    Inventor: John G. Williams

    Abstract: A landing zone designation system is provided that includes a master and a slave landing strobes. A detector on an aircraft can detect master and slave optical signals, and a processor can be coupled to the detector to compute placement of the aircraft relative to the master and slave landing strobes. A method is provided for designating a landing zone for an aircraft. The method includes emitting first and second optical signals, where a determination is made whether the aircraft is to land at a first landing zone or a second landing zone depending on a difference between the first optical signal and the second optical signal. A distance to landing within the determined first landing zone or the second landing zone can also be determined.

    Landing zone designation system and method

    公开(公告)号:US10818191B2

    公开(公告)日:2020-10-27

    申请号:US16371751

    申请日:2019-04-01

    Inventor: John G. Williams

    Abstract: A landing zone designation system is provided that includes a master and a slave landing strobes. A detector on an aircraft can detect master and slave optical signals, and a processor can be coupled to the detector to compute placement of the aircraft relative to the master and slave landing strobes. A method is provided for designating a landing zone for an aircraft. The method includes emitting first and second optical signals, where a determination is made whether the aircraft is to land at a first landing zone or a second landing zone depending on a difference between the first optical signal and the second optical signal. A distance to landing within the determined first landing zone or the second landing zone can also be determined.

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