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Fundamentals of the Polarimetric Navigation System

机译:极化导航系统的基本原理

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The article deal with the development of a polarimetric navigation system, which would determine the relative attitude and position of airplanes. The detailed analysis of existing navigation systems is shown that the main direction of increase the safety of airplanes flights is forecasting and prevention of airplanes collisions by optimization of the relative trajectory of their flight. It has been shown that this can be achieved by determining the relative attitude and position of airplanes. The paper proposes a polarimetric principle for determining the relative attitude and position of the airplanes to each other, as well as, the navigation system, that implements it. The paper also presents the algorithm of the proposed system's operation and the formulas for predicting possible collisions, as well as, recommendations for changing the airplane's relative flight trajectory to prevent a collision. The results of mathematical modeling of the proposed system showed that the formulas for finding the computational parameters have a simple form, which significantly reduces the load on the computing system. The proposed system, potentially, allows determining the relative angles of roll and course, the relative linear deviations in course and height, the relative azimuth in the horizontal and vertical planes with high accuracy and sensitivity.
机译:本文讨论了极化导航系统的发展,该系统将确定飞机的相对姿态和位置。对现有导航系统的详细分析表明,提高飞机飞行安全性的主要方向是通过优化飞机飞行的相对轨迹来预测和防止飞机碰撞。已经表明,这可以通过确定飞机的相对姿态和位置来实现。本文提出了一种极化原理,用于确定飞机彼此之间的相对姿态和位置,以及实现该相对位置的导航系统。本文还介绍了拟议系统的运行算法和预测可能发生的碰撞的公式,并提出了更改飞机相对飞行轨迹以防止发生碰撞的建议。所提出系统的数学建模结果表明,用于找到计算参数的公式具有简单的形式,从而大大减轻了计算系统的负担。所提出的系统可能潜在地以高精度和灵敏度来确定侧倾和航向的相对角度,航向和高度的相对线性偏差,水平和垂直平面中的相对方位角。

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