2021
DOI: 10.1109/access.2021.3092515
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Dual-Channel and Bidirectional Neural Network for Hypersonic Glide Vehicle Trajectory Prediction

Abstract: Different from traditional aircraft, hypersonic glide vehicles (HGVs) possess stronger maneuverability and a higher flight speed (generally higher than 5 Mach), making trajectory prediction very complicated. Several works have been conducted in this field, which usually analyze the motion characteristics of the HGV first and then use a Kalman filter to track and predict the trajectory. In this way, the accuracy of prediction depends on how to model the control parameters of the target vehicle. The core idea of… Show more

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Cited by 20 publications
(8 citation statements)
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“…• Trajectory prediction is divided into two parts: linear and nonlinear. For example, Xie et al (2021) applied a recurrent neural network with bidirectional gated recurrent units to the nonlinear part, and a single-layer perceptron to the linear part. applied the seq2seq architecture to the nonlinear part and also a single-layer perceptron to the linear part.…”
Section: Hgv Trackingmentioning
confidence: 99%
“…• Trajectory prediction is divided into two parts: linear and nonlinear. For example, Xie et al (2021) applied a recurrent neural network with bidirectional gated recurrent units to the nonlinear part, and a single-layer perceptron to the linear part. applied the seq2seq architecture to the nonlinear part and also a single-layer perceptron to the linear part.…”
Section: Hgv Trackingmentioning
confidence: 99%
“…where S mili S mlli represent the position of the i − th predicted start point and last point in a batch, S oili S olli represent the position of the i − th observed start point and last point in a batch, and N represents the number of batches in Equation ( 31); ξ mi is the i − th modified maneuver parameter sequence in a batch, and ξ fi is the i − th filtering maneuver parameter sequence in a batch in Equation ( 32); ξ pi is the i − th modified maneuver parameter sequence in a batch, and ξ di is the i − th generated maneuver parameter sequence in a batch in Equation (33). l cls , p cls , respectively, represent the one-hot value of label classification and prediction classification in Equation (34).…”
Section: Modification Of the Initial And Last Point Positionmentioning
confidence: 99%
“…Yang et al [32] modified the trajectory prediction error based on the generalized regression neural network (GRNN), by which the accurately predicted trajectory could be obtained. Li et al [33] combined the neural network and Kalman filter, based on the filtering result obtained the predicted trajectory. Cai et al [34] established trajectory data sets of different maneuver modes for hypersonic targets and realized the classification and prediction of hypersonic glide target trajectory by using LSTM.…”
Section: Introductionmentioning
confidence: 99%
“…Neural network prediction [17,18] and regression analysis theory [19,20] are two typical types of data-based prediction methods. To solve the trajectory prediction problem of HGV under complex manoeuvring patterns, reference [21] proposed a method to capture the hybrid dependence between short-term and long-term manoeuvring patterns using a dual-channel bidirectional neural network to intelligently predict the trajectory of HGV in undetectable regions. In the reference [22], a model for predicting target acceleration information using regression integrated sliding average was proposed to solve the trajectory prediction problem for variable manoeuvre HGV targets.…”
Section: Introductionmentioning
confidence: 99%