发明名称 AIRBORNE VISIBILITY INDICATOR SYSTEM AND METHOD
摘要 <p>A system for providing an objective visibility measurement to a flight crew preferably includes a LIDAR system (100), an evaluation unit (150), and a crew interface (200). In at least one embodiment, the system includes the capability of compensating for aircraft turns such that the absolute direction of the visibility reading remains constant through the maneuver. A method for providing an objective visibility reading to a flight crew preferably includes tacking a visibility reading (S820, S920); providing the visibility reading to the flight crew (S830, S930); and notifying the flight crew when the visibility has decreased to and/or less than a minimum visibility threshold (S840).</p>
申请公布号 WO2006049643(A2) 申请公布日期 2006.05.11
申请号 WO2005US11188 申请日期 2005.04.05
申请人 U.S. GOVERNMENT AS REPRESENTED BY THE SECRETARY OF ARMY;ESTRADA III, ARTHUR;PERSSON, JAMES, L. 发明人 ESTRADA III, ARTHUR;PERSSON, JAMES, L.
分类号 G08B21/00 主分类号 G08B21/00
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