用于目标轨迹跟踪和外推的改进型可变结构交互多模型

IF 1.1 4区 工程技术 Q3 ENGINEERING, AEROSPACE International Journal of Aerospace Engineering Pub Date : 2024-05-16 DOI:10.1155/2024/2583156
Xuanming Ren, Xinmin Tang, Yang Zhou, Xiangmin Guan
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引用次数: 0

摘要

为了改善传统变结构交互多模型(VSIMM)算法计算时间长的问题,提高目标预测和外推的精度,我们将自动监视广播(ADS-B)捕获的目标状态和飞行意图信息作为模型的先验信息,并结合 VSIMM 理论框架,设计了意图变结构交互多模型(INT-VSIMM)算法。首先,分解目标在飞行阶段的运动模式,建立完整的运动模型集。其次,根据有向图切换原理,设计了以 "硬 "切换为主、"软 "切换为辅的模型集切换方法。最后,利用 INT-VSIMM 算法对目标飞行器进行轨迹跟踪,并根据目标状态估计进行短期轨迹外推。仿真结果表明,基于 INT-VSIMM 算法的目标跟踪性能计算时间优于现有的比较方法,外推轨迹的短期误差较小,可以满足冲突检测的需要。
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Improved Variable Structure Interacting Multimodels for Target Trajectory Tracking and Extrapolation
To improve the lengthy computation time of conventional variable structure interacting multiple model (VSIMM) algorithm and increase the precision of target prediction and extrapolation, the target state and flight intent information captured by the Automatic Dependent Surveillance-Broadcast (ADS-B) are used as the model’s prior information; combining this information with VSIMM theoretical framework, we purpose an intent variable structure interacting multiple model (INT-VSIMM) algorithm. Firstly, the motion pattern of the target in the flight phase of the flight path is decomposed, and complete sets of motion models are established. Secondly, according to the principle of directed graph switching, a model set switching method is designed, which is mainly based on “hard” switching and supplemented by “soft” switching. Finally, the INT-VSIMM algorithm is used to track the trajectory of the target aircraft, and short-term trajectory extrapolation is performed based on the target state estimation. The simulation results show that the target tracking performance computational time based on the INT-VSIMM algorithm is superior to the comparative existing methods, and the extrapolated trajectory has less error in the short term, which can satisfy the needs of conflict detection.
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来源期刊
CiteScore
2.70
自引率
7.10%
发文量
195
审稿时长
22 weeks
期刊介绍: International Journal of Aerospace Engineering aims to serve the international aerospace engineering community through dissemination of scientific knowledge on practical engineering and design methodologies pertaining to aircraft and space vehicles. Original unpublished manuscripts are solicited on all areas of aerospace engineering including but not limited to: -Mechanics of materials and structures- Aerodynamics and fluid mechanics- Dynamics and control- Aeroacoustics- Aeroelasticity- Propulsion and combustion- Avionics and systems- Flight simulation and mechanics- Unmanned air vehicles (UAVs). Review articles on any of the above topics are also welcome.
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