Airborne navigation database(NavDB)coding directly affects the result of analysis on the instrument flight procedure by the modern aircraft flight management computer(FMC).A reasonable flight track transition mode can...Airborne navigation database(NavDB)coding directly affects the result of analysis on the instrument flight procedure by the modern aircraft flight management computer(FMC).A reasonable flight track transition mode can improve the track tracking accuracy and flight quality of the aircraft.According to the path terminator(PT)and track transition characteristics of the performance based navigation(PBN)instrument flight procedure and by use of the world geodetic system(WGS)-84 ellipsoidal coordinate system,the algorithms for“fly by”and“fly over”track transition connections are developed,together with the algorithms for coordinates of fix-to-altitude(FA)altitude termination point and heading-to-an-intercept(VI)track entry point and for track transition display of the navigation display(ND).According to the simulation carried out based on the PBN instrument approach procedure coding of a certain airport and the PBN route data at a high altitude,the algorithm results are consistent with the FMC-calculated results and the actual ND results.展开更多
指出了当前民航业传统的飞行程序已逐渐被基于性能导航(Performance based navigation,PBN)飞行程序所替代,PBN进离场及进近航线设计过程中,可以灵活处理,导航点的设置不用过于依赖地面导航台的位置。然而,PBN进近程序若采用气压表垂直...指出了当前民航业传统的飞行程序已逐渐被基于性能导航(Performance based navigation,PBN)飞行程序所替代,PBN进离场及进近航线设计过程中,可以灵活处理,导航点的设置不用过于依赖地面导航台的位置。然而,PBN进近程序若采用气压表垂直引导的类精密进近方式,则需要考虑到机场的温度限制,一般温度越低,气压越低,因此,飞机上指示的高度比实际飞行高度要高,超障余度不足,可能导致飞机低飞与障碍物发生碰撞的危险。根据DOC8168文件规范,通过举例研究了PBN基于气压高度表垂直引导的进近程序如何设计,并给出了设计流程方案,该方案有利于Baro-VNAV气压式垂直导航的进近程序设计,并具有很好的可靠性和适用性。展开更多
基金supported by the National Natural Science Foundation of China(u2133209)。
文摘Airborne navigation database(NavDB)coding directly affects the result of analysis on the instrument flight procedure by the modern aircraft flight management computer(FMC).A reasonable flight track transition mode can improve the track tracking accuracy and flight quality of the aircraft.According to the path terminator(PT)and track transition characteristics of the performance based navigation(PBN)instrument flight procedure and by use of the world geodetic system(WGS)-84 ellipsoidal coordinate system,the algorithms for“fly by”and“fly over”track transition connections are developed,together with the algorithms for coordinates of fix-to-altitude(FA)altitude termination point and heading-to-an-intercept(VI)track entry point and for track transition display of the navigation display(ND).According to the simulation carried out based on the PBN instrument approach procedure coding of a certain airport and the PBN route data at a high altitude,the algorithm results are consistent with the FMC-calculated results and the actual ND results.
文摘指出了当前民航业传统的飞行程序已逐渐被基于性能导航(Performance based navigation,PBN)飞行程序所替代,PBN进离场及进近航线设计过程中,可以灵活处理,导航点的设置不用过于依赖地面导航台的位置。然而,PBN进近程序若采用气压表垂直引导的类精密进近方式,则需要考虑到机场的温度限制,一般温度越低,气压越低,因此,飞机上指示的高度比实际飞行高度要高,超障余度不足,可能导致飞机低飞与障碍物发生碰撞的危险。根据DOC8168文件规范,通过举例研究了PBN基于气压高度表垂直引导的进近程序如何设计,并给出了设计流程方案,该方案有利于Baro-VNAV气压式垂直导航的进近程序设计,并具有很好的可靠性和适用性。
