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METHOD AND DEVICE OF IMITATION OF TRAJECTORIES OF MOTION OF AIR OBJECTS

机译:模仿空气运动轨迹的方法和装置

摘要

1. A method for simulating the trajectories of air objects by manually entering the initial polar coordinate of the object in the form of bearing P0, distance d0, kob course, the initial velocity νob and subsequent automatic formation of the trajectory of movement in the form of a line segment coming from the point (P0; d0) in the direction kob, until receipt of a signal to the beginning of the maneuver (turn), simultaneous with the introduction of the new course and νob kob movement speed of the object by the time a new rate, with simulated maneuver (turn) by coupling two different linear directed portions motion arc of a circle, which is determined by a rate-radius ωk, which is also given at the beginning of the maneuver, characterized in that the simulation trajectories of objects is carried out by manually entering coordinates of control points of the path of movement indicating the flight velocities at these points and automatic calculation equations motion in three coordinates x (t), y (t), z (t) and speed θ (t) immediately after the data input in the workplace of the operator 5, with subsequent transfer coefficients these equations in block coordinates calculating 6, wherein in response to a request for information about the current position of the object computed its Cartesian coordinates by substituting the time parameter t in equation of motion corresponding to overcome in the time t portion trajectory, which trajectory of aircraft object is represented consisting of elementary segments in the form of line segments, which mate at the angle therebetween φ 90 ° is performed with the exception of the velocity and acceleration jumps matching portions in the form d
机译:1.一种通过手动输入物体的初始极坐标以轴承P0,距离d0,kob航迹,初始速度νob以及随后自动形成形式的运动轨迹来模拟空中物体的轨迹的方法从点(P0; d0)沿kob方向来的线段,直到接收到操纵开始(转弯)的信号,同时引入新的航向和对象的νobkob移动速度通过耦合两个不同的线性有向部分的圆的运动弧来模拟新的速率(转弯)的时间,该弧由速率半径ωk决定,该半径也由机动开始时给出,其特征在于通过手动输入运动路径的控制点坐标(指示这些点的飞行速度)和自动计算方程在三个坐标x中的运动来执行对象的模拟轨迹(t),y(t),z(t)和速度θ(t)紧接在操作员5的工作场所中输入数据之后,这些方程随后以块坐标计算这些方程式6,其中响应于请求为了获得有关物体当前位置的信息,通过将运动参数中的时间参数t替换为对应于在时间t部分轨迹中克服的运动方程来计算其笛卡尔坐标,该飞机物体的轨迹表示为线段形式的基本段除了速度和加速度跳跃匹配部分的形式为d以外,它们之间以φ<90°的角度配对。

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