基于改进动态窗口法的低噪声离场航迹规划研究

Research on Low Noise Departure Trajectory Planning Based on Improved Dynamic Window Method

摘要:

随着民用航空业的迅速发展，绿色航空逐渐成为人们关注的焦点。综合考虑航空器性能、噪声影响、终端区大气环境等因素，提出航空器离场航迹优化方案。针对传统动态窗口法（DWA）在航空器离场航迹规划上无法有效求解的问题，提出一种结合航空器性能的改进动态窗口法，根据航空器性能数据（BADA）和连续爬升运行（CCO）的要求，构建航空器离场性能约束；同时考虑航空器离场时的噪声影响，噪声影响越小则航迹越优；在相同的研究环境下，从影响时长和影响面积角度对不同指标权重下的方法进行分析，选取综合影响最小的方法。根据所选方法，对离场航空器的推力、速度和航径角等性能参数进行分析。结果表明：改进动态窗口法下航迹能够满足航空器离场性能要求。

Abstract:

With the rapid development of civil aviation industry, green aviation has gradually become the focus of people"s attention. Taking into account factors such as aircraft performance, noise impact, and atmospheric environment in the terminal area, an optimization plan for aircraft departure trajectory has been proposed. Aiming at the problem that traditional Dynamic Window Approach (DWA) cannot effectively solve in aircraft departure trajectory planning, an improved Dynamic Window Approach combined with aircraft performance is proposed. Construct aircraft departure performance constraints based on the requirements of Base of Aircraft Data (BADA) and Continuous Climb Operations (CCO). At the same time, considering the noise impact of aircraft departure, the smaller the noise impact, the better the trajectory. Secondly, under the same research environment, analyze the methods with different index weights based on the duration and area of influence, and select the methods with the smallest comprehensive impact. Finally, based on the selected method, analyze the performance parameters such as thrust, speed, and path angle of the departing aircraft. The simulation experiment results show that the trajectory under the improved dynamic window method can meet the requirements of aircraft departure performance.