基于4D轨迹的连续下降作业动态航路速度剖面调整策略设计

Jun Zhang, Gang Xiao, Guoqing Wang
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引用次数: 0

摘要

为了降低高密度空域连续下降作战(CDO)飞行轨迹的不确定性,需要在CDO过程中设计有约束的速度剖面,并利用四维(4D)轨迹预测和飞行速度调整技术来满足空间和时间约束。提出了一种多约束条件下基于四维轨迹的大型飞机实时飞行轨迹管理策略。为了提高可行控制到达时间窗口的预测精度,提出了一种基于飞机性能数据和飞机意图模型的计算方法。最后,提出了一种基于飞机运动学模型的航路动态速度调整策略,通过基于性能空域和CTA程序实现了CDO的最优飞行轮廓和到达目标所需时间。为了验证本文算法的有效性,在MATLAB平台上对某型国产飞机进行了快速仿真。仿真结果验证了本文提出的实时轨迹管理算法和动态航路速度剖面调整策略能够为航空公司提供面向定时到达的精确飞行速度控制能力。
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Dynamic En-route Speed Profile Adjustment Strategy Design for Continuous Descend Operations Based on 4D Trajectory
Aiming to reduce the uncertainty of the trajectory of Continuous Descend Operations (CDO) in high-density airspace, it is necessary to design a constrained speed profile during the CDO procedures, and use 4-Dimensional (4D) trajectory prediction and flight speed adjustment technology to meet the constraints on both space and time. This paper presents a large aircraft real-time flight trajectory management strategy based on 4D trajectory under multi-constraint conditions. To improve the prediction accuracy of the feasible Controlled Time of Arrival (CTA) window, a calculation method based on aircraft performance data and aircraft intention model is proposed. Finally, a dynamic en-route speed adjustment strategy based on the aircraft kinematics model is proposed, and the optimal flight profile and the required time of arrival objectives of the CDO are achieved with the performance-based airspace and CTA procedures. To demonstrate the validation of the algorithms given in the paper, the fast-time simulation based on a type of domestically-made aircraft is operated by the MATLAB platform. The simulation results verified that the real-time trajectory management algorithms and dynamic en-route speed profile adjustment strategy proposed in this paper could provide a precise flight speed control capability oriented to timing arrival for airlines.
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