基于PEP的起飞一发失效应急程序研究

Design of Engine out Standard Instrument Procedure Based on PEP Software

对航迹计算研究中的常用方法进行了简要叙述,给出了民航飞机起飞一发失效时飞行航迹的组成,并建立了飞机一发失效时的运动受力模型。在净空条件差、地形复杂地区,提出基于PEP的起飞一发失效应急程序设计,并以华南某机场为例,进行了基于PEP的起飞一发失效应急程序设计,得出所设计的一发失效程序准确、可靠,对机场航行服务研究和航空公司性能人员具有一定的指导作用。

Some algorithms which are often used in track computation are briefly described in this paper, and the composition of the flight track of one engine flame out is also introduced. When one engine flame out occurs, the forces acting on the plane are analyzed. In some regions where terrain is complicated, the design of one engine flame out standard instrument procedure （EOSID） based on PEP software is put forward, and taking an example of an airport located in the south of China, an EOSID is designed based on PEP. According to the result, this procedure is reliable and correct. Therefore it provides some help for the researchers who work in airlines and airport construction insti- tute.