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基于混杂系统理论的无冲突4D航迹预测

韩云祥 汤新民 韩松臣

韩云祥, 汤新民, 韩松臣. 基于混杂系统理论的无冲突4D航迹预测[J]. 西南交通大学学报, 2012, 25(6): 1069-1074. doi: 10.3969/j.issn.0258-2724.2012.06.025
引用本文: 韩云祥, 汤新民, 韩松臣. 基于混杂系统理论的无冲突4D航迹预测[J]. 西南交通大学学报, 2012, 25(6): 1069-1074. doi: 10.3969/j.issn.0258-2724.2012.06.025
HAN Yunxiang, TANG Xinmin, HAN Songchen. Conflict-Free 4D Trajectory Prediction Based on Hybrid System Theory[J]. Journal of Southwest Jiaotong University, 2012, 25(6): 1069-1074. doi: 10.3969/j.issn.0258-2724.2012.06.025
Citation: HAN Yunxiang, TANG Xinmin, HAN Songchen. Conflict-Free 4D Trajectory Prediction Based on Hybrid System Theory[J]. Journal of Southwest Jiaotong University, 2012, 25(6): 1069-1074. doi: 10.3969/j.issn.0258-2724.2012.06.025

基于混杂系统理论的无冲突4D航迹预测

doi: 10.3969/j.issn.0258-2724.2012.06.025
基金项目: 

国家自然科学基金资助项目(61174180)

中央高校基本科研业务费专项资金资助-江苏省普通高校研究生科研创新计划 资助项目(CXLX11_0210)

江苏省自然科学基金资助项目(BK2010502)

Conflict-Free 4D Trajectory Prediction Based on Hybrid System Theory

  • 摘要: 为增大空域容量,在战略航迹规划阶段,设定航空器爬升、下降和平飞3个飞行状态和7组高度和速度参数规划航空器4D航迹.基于不同航段的航空器动力学模型,采用混杂系统理论, 建立了不同航段之间的状态切换模型,以及同一航段内航空器质量、空速、高度和航程连续变化的航空器运行状态演化模型. 通过调整航空器到达时刻和飞行速度,规划了多航空器无冲突4D航迹.算例仿真结果表明,在满足航空器性能约束的前提下,用混杂系统递推法规划的航空器起飞4D航迹计算时间在3 s以内;这两个模型准确反映了航空器在水平剖面和垂直剖面内的飞行状态变化;本文提出的航空器无冲突航迹规划方法是有效的.

     

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出版历程
  • 收稿日期:  2011-05-20
  • 刊出日期:  2012-12-25

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