| 摘要 |
<p>PURPOSE:To enable a fast and accurate flight control to be realized by a method wherein it is decided if a flight route calculated in response to various data of launching of an airframe and a present weather condition reaches a desired target point without contacting a geometrical barrier, a flight prohibiting region and an airframe detecting radar beam. CONSTITUTION:A vertical lower altitude of an airframe (e) is calculated from a two-dimensional coordinates except an altitude component of a three- dimensional position (c) of the airframe. A geometrical barrier conflict decision device 5 may compare the three-dimensional position (c) of the airframe with the vertical lower altitude (e) so as to decide a conflict (f) of the airframe with the geometrical barrier. A flight prohibition region data input device 6 inputs the flight prohibition data (g) composed of a central line, an altitude width and a lateral width of the flight prohibiting region through an operation of an operator. A flight prohibition region conflict decision device 7 decides a conflict (h) of the flight rought with the flight prohibiting region in response to the three-dimensional position (c) of the aircraft and the flight prohibiting data (g). The device is aircraft sensing radar beam data input device 8.</p> |
