首页> 外文会议>ASME international mechanical engineering congress and exposition >LATERAL NAVIGATION OPTIMIZATION CONSIDERING WINDS AND TEMPERATURES FOR FIXED ALTITUDE CRUISE USING DIJSKTRA'S ALGORITHM
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LATERAL NAVIGATION OPTIMIZATION CONSIDERING WINDS AND TEMPERATURES FOR FIXED ALTITUDE CRUISE USING DIJSKTRA'S ALGORITHM

机译:考虑迪格斯特拉算法的固定海拔巡航风和温度的横向导航优化

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Optimizing the flight trajectory is a goal that will minimize fuel consumption and time related costs. Lateral Navigation (LNAV) has been investigated as part of identifying optimal trajectories. Winds and temperature have an important influence in the cost of a flight. Tail winds and low temperatures are desired, as both reduce flight costs. Implementing algorithms to locate where these favorable conditions exist close to the defined trajectory of a given flight will help to achieve optimal flight trajectories. These algorithms are to be implemented in an FMS using an aircraft model which is normally given in the form of a Performance Database (PDB). The approach given in this paper uses Dijsktra's algorithm. This method is part of the graph-search techniques. The search area is defined by discretizing the cruise trajectory and defining adjacent waypoints, forming a grid where the possible trajectories are created. The algorithm requires the aircraft's gross weight at the top of climb (TOC), the location of the top of descent (TOD), and the desired cruise speed and altitude. The related costs are calculated using the PDB's model for two different commercial aircraft at a constant altitude and at a constant indicated mach. To minimize the costs, the algorithm considers the fuel burned, the flight time and the cost index (CI). The temperature and winds in the trajectory are obtained from the Canadian weather forecast (Environment Canada). Wind influence is taken into account by adding it to the ground speed, based on its direction regarding the aircraft's trajectory heading. The effect of temperature is considered in the PDB. Generated trajectories are compared against the geodesic (or great circle) route.
机译:优化飞行轨迹是将燃油消耗和与时间相关的成本降至最低的目标。横向导航(LNAV)已作为确定最佳轨迹的一部分进行了研究。风和温度对飞行成本有重要影响。期望尾风和低温,因为两者都降低了飞行成本。实施算法来定位这些有利条件的存在位置,使其接近给定飞行的定义轨迹,将有助于实现最佳飞行轨迹。这些算法将在FMS中使用飞机模型来实现,该模型通常以性能数据库(PDB)的形式给出。本文给出的方法使用Dijsktra算法。此方法是图搜索技术的一部分。通过离散化巡航轨迹并定义相邻的航路点,形成一个在其中创建可能轨迹的网格,来定义搜索区域。该算法要求飞机的总重量位于爬升顶部(TOC),下降顶部的位置(TOD)以及所需的巡航速度和高度。使用PDB模型对两架不同的商用飞机在恒定的高度和恒定的指示马赫数下计算相关成本。为了使成本最小化,该算法考虑了燃烧的燃料,飞行时间和成本指数(CI)。轨迹中的温度和风是从加拿大天气预报(加拿大环境部)获得的。根据风对飞机轨迹方向的影响,将风影响添加到地面速度中,从而将风影响考虑在内。在PDB中考虑了温度的影响。将生成的轨迹与测地线(或大圆)路线进行比较。

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