2019
DOI: 10.1109/access.2019.2899678
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Multiple Model Tracking for Hypersonic Gliding Vehicles With Aerodynamic Modeling and Analysis

Abstract: The multiple model tracking methods for hypersonic gliding vehicles (HGVs), which improves the design of tracking model-set is proposed in this paper. Different from the traditional tracking method with dynamic pressure models, the proposed method refines the model-set by modeling and analyzing the specific aerodynamic characteristics of the HGVs. Based on the aerodynamic model of the vehicle, the novel tracking models are established and the multiple model tracking methods are adopted. The uniform modelsets a… Show more

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Cited by 17 publications
(11 citation statements)
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“…(2) The maximum lift-to-drag ratio of the HTV-2-like HGV is around 4, which is in accordance with the results of the existing literature [27]. (3) In general, the lift-drag ratio of the HGV positively correlates with the angle of attack. (4) The lift-to-drag ratios of HGV are basically independent of the Mach number.…”
Section: A Parametric Model Of Htv-2-like Hgvssupporting
confidence: 87%
See 1 more Smart Citation
“…(2) The maximum lift-to-drag ratio of the HTV-2-like HGV is around 4, which is in accordance with the results of the existing literature [27]. (3) In general, the lift-drag ratio of the HGV positively correlates with the angle of attack. (4) The lift-to-drag ratios of HGV are basically independent of the Mach number.…”
Section: A Parametric Model Of Htv-2-like Hgvssupporting
confidence: 87%
“…Generally, trajectory tracking and estimation are fulfilled through a filter, which combines measured data received from the radar and that of the reference model [2]. Accordingly, the reference model has a significant impact on the estimation accuracy of the trajectory [3], [4]. This is especially more pronounced for state variables, which cannot be measured directly.…”
Section: Introductionmentioning
confidence: 99%
“…In this paper, the IMM-UKF algorithm [37] is used to track observed 20, 000 trajectories at the position (0.4 °E, 0 °N, 100). Assuming that the observational error of radar is Gaussian error with ½ð30mÞ 2 , ð0:1 °Þ2 , ð0:1 °Þ2 , the original trajectory data of all trajectories from 400 to 600 s are generated as observation data set and filtering data set.…”
Section: Data Setmentioning
confidence: 99%
“…HGV is an aircraft with a speed above Mach 5 and flying in near space [1]. Compared with a conventional ballistic missile, HGV has stronger maneuverability and can strike any target in the world within two hours [2].…”
Section: Introductionmentioning
confidence: 99%