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4D Trajectory Prediction of Aircraft Taxiing Based on Fitting Velocity Profile 基于拟合速度剖面的飞机滑行四维轨迹预测
Pub Date : 2015-07-22 DOI: 10.1061/9780784479292.001
Xin-min Tang, Long Zhou, Zhiyuan Shen, M. Tang
To improve the overall efficiency and comprehensive support capability of airports, a method of predicting 4D taxiing-trajectory for aircraft on airport surface based on fitting velocity profile is proposed. Firstly, the dynamic model of aircraft taxiing is built, and the concept of nominal velocity profile is introduced. Secondly, DSW algorithm is applied to generate a nominal velocity profile. Furthermore, the average velocity modification parameters are calculated to update taxiing velocity, which is influenced by different aircraft types. According to mapping between nominal velocity and instantaneous velocity based on the dynamic equilibrium equation, instantaneous velocity is updated combining with BADA data. Finally, aircraft taxiing 4D trajectory prediction is achieved. It can more accurately predict arriving aircraft at given position and reduce conflict. Case studies demonstrates that this method reduces 47.3% of the average error between estimated time and actual time when compared with the competing methods based on dynamic models.
为了提高机场的整体效率和综合保障能力,提出了一种基于拟合速度剖面的飞机在机场表面滑行轨迹四维预测方法。首先,建立了飞机滑行动力学模型,引入了名义速度剖面的概念;其次,采用DSW算法生成标称速度剖面;此外,计算平均速度修正参数来更新受不同机型影响的滑行速度。根据动力平衡方程的标称速度与瞬时速度的映射关系,结合BADA数据更新瞬时速度。最后,实现了飞机滑行四维轨迹预测。它可以更准确地预测到给定位置的飞机,减少冲突。实例研究表明,与基于动态模型的竞争方法相比,该方法估计时间与实际时间的平均误差降低了47.3%。
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引用次数: 7
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航空计算技术
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