Electronics and Electrical Engineering and Control

Adaptive tracking model for near space hypersonic jumping gliding target

  • LI Fan ,
  • XIONG Jiajun
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  • 1. Graduate Management Office, Air Force Early Warning Academy, Wuhan 430019, China;
    2. Early Warning Intelligence, Air Force Early Warning Academy, Wuhan 430019, China

Received date: 2018-05-23

  Revised date: 2018-08-06

  Online published: 2018-08-30

Supported by

National High-tech Research and Development Program of China (2015AA7056045, 2015AA8017032P)

Abstract

To address the near space hypersonic jump gliding target tracking problem, an Adaptive Non-zero Mean Sine Wave (ANM-SW) model is proposed on the basis of modeling acceleration as a random process of Sine Wave (SW) autocorrelation. The core of the model is to compensate the mean SW and construct the ANM-SW model; in this process, the state equation of the model is derived. To further analyze the role of mean compensation with this model, the physical nature of adaptive non-zero mean value model is discussed from the perspective of time domain and frequency domain. Furthermore, the system dynamic errors of SW and ANM-SW models status update are deduced taking Kalman filter as the filtering algorithm. In this way, the superiority of ANM-SW model in maneuver adaptation is verified. Finally, the simulation experiments show that compared with SW model, ANM-SW model has certain advantages in tracking accuracy and maneuverability.

Cite this article

LI Fan , XIONG Jiajun . Adaptive tracking model for near space hypersonic jumping gliding target[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018 , 39(12) : 322355 -322355 . DOI: 10.7527/S1000-6893.2018.22355

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