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Determination of Guidance Law for Aviation Obstacles, Computer Program Products, Electronic Systems and Related Aviation

机译:确定航空障碍物,计算机程序产品,电子系统和相关航空的指导法

摘要

This method of determining the guidance law of aircraft obstruction is implemented by the system that determines the guidance law of aircraft obstruction. The aircraft consists of an anti-collision system capable of detecting the collision risk of obstacles and a determination system.The method includes determining (110) slope and speed instructions (VZ ^ U).International Accounting Standards,At least one instruction (VZU instruction) depends on at least one vertical velocity limit.At least one instruction (VZU instruction) having a vertical component in the vertical direction,1. After the collision hazard is detected, each limit value is provided by the collision avoidance system.And according to the prescribed criteria (160).In the determination step, at least one determined instruction (IASU) includes a longitudinal component perpendicular to the vertical direction.
机译:确定飞机障碍物的制导律的这种方法由确定飞机障碍物的制导律的系统实现。该飞机由能够检测障碍物碰撞风险的防撞系统和确定系统组成。该方法包括确定(110)坡度和速度指令(VZ ^ U)。国际会计标准,至少一条指令(VZU指令)取决于至少一条垂直速度限制。至少一条指令(VZ U指令)在垂直方向上具有垂直分量1。在检测到碰撞危险后,由防撞系统提供每个限值,并按照规定的标准(160)。在确定步骤中,至少一个确定的指令(IASU)包括垂直于垂直方向的纵向分量。

著录项

  • 公开/公告号FR3018364A1

    专利类型

  • 公开/公告日2015-09-11

    原文格式PDF

  • 申请/专利权人 THALES;

    申请/专利号FR20140000537

  • 申请日2014-03-04

  • 分类号G05D1/06;G08G5/04;

  • 国家 FR

  • 入库时间 2022-08-21 14:54:07

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