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METHOD FOR DETERMINING THE COURSE aerodynamic targets

机译:确定课程空气动力学目标的方法

摘要

A method of determining the course aerodynamic purposes, comprising the steps that produce the transformation of the measured spherical coordinates in a horizontal Cartesian coordinates are evaluated rate of change of the horizontal cartesian coordinates evaluated auxiliary angle between the velocity vectors change horizontal Cartesian coordinates as the arctangent of the quotient of velocity estimates the changes of the horizontal cartesian coordinates, course objectives wind is uniquely determined by the following algorithm, if the estimate is STI change horizontal cartesian coordinates is greater than zero, the rate is equal to the estimate of the auxiliary angle, if the speed estimate the change of the horizontal cartesian coordinate is less than zero, then the rate equal to the difference between the estimate of the auxiliary angle and an angle of 180 °, if the estimated rate of change of the horizontal cartesian coordinates on the coordinate axis, the positive direction which is the origin of measurement of azimuth and course, greater than zero, and the estimation speed change other horizontal cartesian coordinates is less than zero, then ku pc is the difference between 360 ° and evaluation auxiliary angle if the estimate of the rate change horizontal Cartesian coordinates on a coordinate axis, the positive direction which is the origin of measurement of azimuth and course is less than zero, and the estimation speed change other horizontal cartesian coordinates is greater than zero, then the rate equals the sum of evaluations of the auxiliary angle and the angle of 180 °, characterized in that the coordinate transformation is calculated on the product of the radial velocity-range, the sample obtained produ
机译:一种确定过程空气动力学目的的方法,包括产生水平笛卡尔坐标中的所测球坐标的变换的步骤,通过评估水平笛卡尔坐标的变化率来评估速度矢量之间的辅助角,将水平笛卡尔坐标作为反正切速度的商估计水平笛卡尔坐标的变化,通过以下算法唯一确定航向目标风,如果估计值是STI变化水平笛卡尔坐标的值大于零,则速率等于辅助角的估计,如果速度估计水平笛卡尔坐标的变化小于零,则速率等于辅助角估计与180°角之间的差,如果水平笛卡尔坐标的估计变化率在坐标轴,正方向是方位角和航向的测量原点大于零,并且估计速度变化的其他水平笛卡尔坐标小于零,则ku pc是360°与评估辅助角之间的差,如果速率变化的估计水平笛卡尔坐标在坐标轴上,作为方位角和航向测量起点的正方向小于零,并且其他水平笛卡尔坐标的估计速度变化大于零,则比率等于辅助角和180°角,其特征在于坐标变换是根据径向速度范围乘积计算得到的

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