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面向高超声速滑翔目标的多模型多意图融合轨迹预测

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针对高超声速滑翔目标速度快、机动强导致轨迹预测精度低且窗口有限的问题,提出了一种多模型多意图融合轨迹预测方法.首先从目标的控制规律出发,构建了纵向、侧向解耦的时变预测模型集,以升力参数、阻力参数与倾侧角幅值为特征参数,通过最小二乘法与高斯假设设计纵向模型;以倾侧角符号为特征参数,针对攻击意图、规避禁飞区以及C/S型机动等典型动作设计侧向模型.然后考虑意图距离、航向角与规避禁飞区等因素设计意图代价函数,基于贝叶斯理论推导预测模型与意图的后验概率递推公式,通过多机动模式、多意图的双层次融合提高轨迹预测准确性与鲁棒性.仿真结果表明,该方法能够应对高超声速滑翔目标的复杂机动,有效提高了长时轨迹预测精度.
Trajectory Prediction Based on Multi-model and Multi-intent Fusion for Hypersonic Gliding Targets
To address the problem of low trajectory prediction accuracy and limited prediction window caused by the high speed and strong maneuverability of hypersonic gliding vehicles,a trajectory prediction method based on multi-model and multi-intent fusion is proposed.By analyzing the control mechanism of targets,a time-varying prediction model set with longitudinal and lateral decoupling is constructed.Taking the lift variable,the drag variable and the amplitude of bank angle as the characteristic parameters,longitudinal maneuver models are designed through the least square method and Gaussian assumption.Taking the sign of bank angle as the characteristic parameter,lateral maneuver models are designed for typical actions such as attacking intents,avoiding no-fly zones,C-type and S-type maneuvers.Furthermore,the intent cost function is designed by combining the intent's distance,heading angles and avoiding no-fly zones.The posterior probability recursive formulas of maneuver patterns and intents are derived based on the Bayesian theory.Through double-level fusion of multiple maneuver patterns and multiple intents,the accuracy and robustness of trajectory prediction are improved.Simulation results show that the proposed method can cope with complex maneuvers of hypersonic gliding targets and effectively improve the performance of long-term trajectory prediction.

Hypersonic gliding vehiclesTrajectory predictionManeuver model inferenceIntent inferenceBayesian theory

李佳丽、郭杰、唐胜景

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北京理工大学宇航学院,北京 100081

飞行器动力学与控制教育部重点实验室(北京理工大学),北京 100081

高超声速滑翔飞行器 轨迹预测 机动模式推断 意图推断 贝叶斯理论

国家自然科学基金上海航天科技创新基金(SAST基金)

11572036SAST201711

2024

宇航学报
中国宇航学会

宇航学报

CSTPCD北大核心
影响因子:0.887
ISSN:1000-1328
年,卷(期):2024.45(2)
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