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En-route descent trajectory synthesis for air traffic control automation

机译:用于空中交通管制自动化的航路下降轨迹综合

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This paper discusses en-route trajectory synthesis that is key to the Center-TRACON Automation System developed at NASA Ames for air traffic control automation. Based on trajectories produced in the Trajectory Synthesizer (TS) module, computer advisories are generated that help controllers to produce a safe, efficient, and expeditious flow of traffic for the extended terminal area. TS synthesizes trajectories from the initial position to the final position in the en-route area for one aircraft at a time by integrating a set of simplified point-mass equations. Specifically, TS separates the horizontal path from the vertical trajectory. The horizontal path is constructed from specified waypoints using straight lines and constant-radius turns. The vertical trajectory is divided into a series of flight segments. Three types of flight profiles are defined by connecting selected segments in a pre-determined order: fast, nominal and slow. Each profile can produce a certain range of arrival times. In numerical computations, a second-order Runge-Kutta scheme is used for integrating equations of motion. A regula falsi iterative scheme is employed to determine the speed that will meet a specified arrival time. Two flight scenarios are used to illustrate the TS solution procedure.
机译:本文讨论了航路轨迹综合,这是在NASA Ames开发的用于空中交通管制自动化的Center-TRACON自动化系统的关键。根据在轨迹合成器(TS)模块中产生的轨迹,生成计算机咨询,以帮助控制器为扩展的终端区域产生安全,高效且迅速的交通流。 TS通过集成一组简化的点质量方程式,一次对一架飞机的航路区域中从初始位置到最终位置的轨迹进行合成。具体而言,TS将水平路径与垂直轨迹分开。使用直线和恒定半径的转弯从指定的航路点构建水平路径。垂直轨迹分为一系列飞行段。通过以预定顺序连接选定的航段来定义三种类型的飞行曲线:快速,标称和缓慢。每个配置文件可以产生一定范围的到达时间。在数值计算中,二阶Runge-Kutta方案用于积分运动方程。使用规则伪造迭代方案来确定将满足指定到达时间的速度。使用两个飞行方案来说明TS解决方案的过程。

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