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FIXED-WING AIRCRAFT, FIXED-WING AIRCRAFT SYSTEM, AND LANDING METHOD FOR FIXED-WING AIRCRAFT

机译:固定翼飞机,固定翼飞机系统以及固定翼飞机的着陆方法

摘要

PROBLEM TO BE SOLVED: To solve a problem that although an uninhabited fixed-wing aircraft is transferred to a phase of glide landing after passing through a landing intrusion point, it extremely excessively passing a landing point on a flight plan by influence of tail wind.;SOLUTION: When it is calculated that a presumption landing point excessively passes a set landing point, landing intrusion is performed again. At the execution, the landing intrusion point is moved in a direction left from a landing point by an excessive degree and also cope with tail wind. Further, by regulating behavior of re-approach, landing at a narrow space area is attained. Further, at the intrusion to the landing intrusion point having a passing determination condition for linearly intruding it to the landing point, linear intrusion is attained by performing flight along a circumference of a circle in which a line connecting the landing intrusion point and the landing point becomes a tangent.;COPYRIGHT: (C)2011,JPO&INPIT
机译:需要解决的问题:为了解决一个问题,尽管无人驾驶的固定翼飞机在经过着陆点后进入了滑行着陆阶段,但由于尾风的影响,它在飞行计划中过分地过了着陆点。 ;解决方案:当计算出推定的着陆点过多地超过了设定的着陆点时,再次执行着陆侵入。在执行时,着陆点在离开着陆点的方向上过度移动,并且还应对尾风。此外,通过调节重新接近的行为,实现了在狭窄空间区域的着陆。此外,在具有通过以线性方式将其侵入到着陆点的通过条件的到达着陆点的侵入时,通过沿着圆的圆周飞行来实现线性侵入,在该圆周中,连接着陆着入点和着陆点的线成为切线。;版权所有:(C)2011,JPO&INPIT

著录项

  • 公开/公告号JP2010269724A

    专利类型

  • 公开/公告日2010-12-02

    原文格式PDF

  • 申请/专利权人 HITACHI LTD;

    申请/专利号JP20090124145

  • 申请日2009-05-22

  • 分类号B64D45/04;B64C13/18;

  • 国家 JP

  • 入库时间 2022-08-21 18:22:00

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