CAJ | 학술논문

针对传统跟踪算法跟踪临近空间高超声速目标时计算量大、跟踪精度低的问题，提出了一种变结构多模型跟踪算法。在分析传统跟踪算法的基础上，建立了一种变转移概率、变模型数量的目标模型，通过目标运动状态辨识方法，确定目标飞行阶段，并选择相应滤波模型和模型转移概率，实现变结构多模型跟踪。 Monte Carlo仿真结果表明：新算法能够实现对临近空间高超声速飞行器的有效跟踪，跟踪性能比传统变结构多模型跟踪算法更加优越，具有一定实用性和可推广性。
침대전통근종산법근종림근공간고초성속목표시계산량대、근종정도저적문제，제출료일충변결구다모형근종산법。재분석전통근종산법적기출상，건립료일충변전이개솔、변모형수량적목표모형，통과목표운동상태변식방법，학정목표비행계단，병선택상응려파모형화모형전이개솔，실현변결구다모형근종。 Monte Carlo방진결과표명：신산법능구실현대림근공간고초성속비행기적유효근종，근종성능비전통변결구다모형근종산법경가우월，구유일정실용성화가추엄성。
Aiming at the problem that the traditional tracking algorithm has large amount of calculation and low accuracy while tracking near space hypersonic target, a kind of variable structure multiple model tracking algorithm was proposed. Established a kind of variable probability and variable model number target model on the basis of analyzing the traditional tracking algorithm, identified the target flight phase with the target motion state identification method, and selected the appropriate filter model and the model transition probability to realize variable structure multiple model tracking. The Monte Carlo simulation results show that, the new algorithm can realize tracking the near space hypersonic vehicle effectively, and the tracking performances are superior to the traditional variable structure multiple model tracking algorithm, it has certain practicability and popularization.