首页> 外文会议>Congress of the International Council of the Aeronautical Sciences;ICAS 2008 >ALGORITHM AND OPERATIONAL CONCEPT FOR RESOLVING SHORT-RANGE CONFLICTS
【24h】

ALGORITHM AND OPERATIONAL CONCEPT FOR RESOLVING SHORT-RANGE CONFLICTS

机译:解决小范围冲突的算法和操作概念

获取原文

摘要

The paper describes an algorithm for computing horizontal resolution trajectories with a limit on bank angle. If loss of separation can be avoided, the algorithm generates a set of maneuvers that achieves or exceeds the specified minimum separation. The maneuvers consist of turns to a specified heading followed by straight-line flight. Both single aircraft and cooperative maneuvers are generated. In cooperative maneuvers both conflict aircraft simultaneously execute resolution maneuvers, which expedite the resolution process compared to single aircraft maneuvers. If loss of separation is unavoidable for a specified bank angle limit, the method chooses the maneuver that maximizes the minimum separation during the turns. The characteristics of the resolution trajectories have been analyzed in a parameter space comprising initial positions, encounter angle, airspeed, predicted minimum separation, and bank angle. Analysis of resolutions for sets of initial conditions provided a road map for the design of an algorithm. A conceptual design of a system is described that resolves close-in conflicts automatically by up-linking resolution advisories to aircraft. Controllers have the option to assign detected conflicts to be resolved by the system. The system also has the authority to uplink resolution advisories to the aircraft without prior controller approval if time to loss of separation falls below a threshold value. The Mode S Specific Services data link is well suited for up-linking resolution advisories to the conflict aircraft. Deployment of the system could be an initial step in building the next-generation air traffic control system.
机译:该论文描述了一种用于计算具有倾斜角限制的水平分辨率轨迹的算法。如果可以避免分离损失,该算法将生成一组达到或超过指定最小分离的操作。演习包括转弯到指定的航向,然后进行直线飞行。既产生了单飞机,也产生了合作演习。在合作机动中,两架冲突飞机同时执行决议机动,与单机机动相比,这加快了决议过程。如果在指定的倾斜角限制下不可避免地会出现间距损失,则该方法将选择在转弯期间使最小间距最大化的操作。在一个参数空间中分析了分辨率轨迹的特性,该参数空间包括初始位置,相遇角,空速,预测的最小间隔和倾斜角。对初始条件集的分辨率的分析为算法设计提供了路线图。描述了一种系统的概念设计,该系统通过将解决方案建议链接到飞机来自动解决近距离冲突。控制器可以选择分配要由系统解决的检测到的冲突。如果失去间隔的时间降到阈值以下,则该系统还具有未经飞机师同意而将分辨率建议咨询给飞机的权限。模式S特定服务数据链接非常适合将解决方案建议上行链接到冲突飞机。系统的部署可能是构建下一代空中交通管制系统的第一步。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号