Planning the Optimal Reference Flight Path of an Aircraft Using a Terrain Map

Q4 Engineering
N. B. Agayev, Q. H. Orujov, N. N. Kalbiyev
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引用次数: 0

Abstract

In connection with the development of aviation technology, the expansion of the functionality of modern aircraft and the complication of the tasks being solved, additional stringent requirements are imposed on the accuracy of air navigation. Along with high accuracy, navigation autonomy is also required. The autonomy of aircraft navigation implies the navigation of an aircraft without the use of active radar facilities. In this article, to calculate the optimal reference flight path of an aircraft in a horizontal plane, the Bellman dynamic programming method is proposed using a digital terrain map. A technique, algorithms have been developed, and a numerical experiment has been carried out using fragments of a digital terrain map. High accuracy and autonomy of navigation are necessary, among other things, to ensure stealth (invisibility) of aircraft by ground-based radar facilities of a potential enemy in low-altitude flight mode. The best stealth of an aircraft flight in a low-altitude flight mode is achieved not only by flying around, but also by avoiding obstacles, due to the shielding properties of the earth’s surface. Autonomy of navigation provides periodic correction of the reference flight path during long-term flight, and high accuracy prevents aircraft collisions with the earth’s surface in low-altitude flight mode. The purpose of this work is to select the optimal reference trajectory (route) of an aircraft flight in the low-altitude flight mode. This article discusses a method developed based on the principle of dynamic programming for calculating the reference flight path in the horizontal plane depending on the DEM and the implementation of the algorithm based on the proposed method with a specific numerical example. The method makes it possible to calculate the optimal flight route, which provides the greatest secrecy of the aircraft in the low-altitude flight mode using the screening properties of the earth’s surface irregularities. 
利用地形图规划飞机最优参考飞行路径
随着航空技术的发展、现代飞机功能的扩大和正在解决的任务的复杂化,对空中导航的准确性提出了更严格的要求。除了高精度之外,还需要导航的自主性。飞机自主导航是指飞机在不使用主动雷达设备的情况下进行导航。为了计算飞机在水平面上的最优参考飞行路径,提出了基于数字地形图的Bellman动态规划方法。开发了一种技术和算法,并利用数字地形图的碎片进行了数值实验。为了确保飞机在低空飞行模式下被潜在敌人的地面雷达设施隐形(隐身),高精度和自主导航是必要的。在低空飞行模式下,由于地球表面的屏蔽特性,飞机的最佳隐身性不仅要通过飞行,还要通过避开障碍物来实现。导航的自主性提供了长期飞行时对参考飞行路径的周期性修正,并且在低空飞行模式下,高精度防止了飞机与地球表面的碰撞。本工作的目的是选择飞机在低空飞行模式下飞行的最优参考轨迹(航路)。本文讨论了一种基于动态规划原理的基于DEM计算水平面参考航迹的方法,并结合具体的数值算例给出了基于该方法的算法实现。该方法可以计算出最佳飞行路线,利用地球表面不规则性的屏蔽特性,为飞机在低空飞行模式下提供最大的保密性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Mekhatronika, Avtomatizatsiya, Upravlenie
Mekhatronika, Avtomatizatsiya, Upravlenie Engineering-Electrical and Electronic Engineering
CiteScore
0.90
自引率
0.00%
发文量
68
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