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:侧向导航优化考虑使用Dijkstra算法的固定高度巡航风和温度

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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:优化飞行轨迹是一种最小化燃料消耗和时间相关成本的目标。作为识别最佳轨迹的一部分,已经调查了横向导航(LNAV)。风和温度对飞行成本具有重要影响。需要尾风和低温,因为减少飞行成本。实现算法以定位在接近给定飞行的定义轨迹附近存在的位置,将有助于实现最佳飞行轨迹。这些算法将使用通常以性能数据库(PDB)的形式给出的飞机模型在FMS中实现。本文给出的方法使用Dijsktra的算法。此方法是图形搜索技术的一部分。搜索区域是通过离散巡航轨迹并定义相邻航点来定义的,形成形成可能的轨迹的网格。该算法要求飞机在爬升顶部(TOC)的总重量,下降(TOD)的位置,以及所需的巡航速度和高度。相关成本使用PDB模型在恒定的高度和恒定的指定马赫以恒定的高度和两个不同的商用飞机进行计算。为了最大限度地减少成本,该算法考虑燃烧的燃料,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)获得的。基于其关于飞机的轨迹标题的方向,通过将风力影响到地面速度来考虑风力影响。在PDB中考虑温度的影响。将生成的轨迹与测地(或大圈)路线进行比较。

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