TY - JOUR
T1 - Online time-varying navigation ratio identification and state estimation of cooperative attack
AU - Wang, Yinhan
AU - Wang, Jiang
AU - Fan, Shipeng
AU - Li, Ling
N1 - Publisher Copyright:
© 2023 Elsevier Masson SAS
PY - 2023/5
Y1 - 2023/5
N2 - An online navigation ratio identification model based on the gated recurrent unit (GRU) and a state estimation extended Kalman filter (EKF) are proposed under the scenario in which multiple enemy missiles attack a stationary target using a time-cooperative guidance law. The navigation ratio identification is solved as a dynamic problem, and the time-varying navigation ratios of each missile, instead of the effective navigation constants and cooperative gains, are identified in this paper. In other words, the simplified assumption that the true value is within a known finite set, which is generally adopted in a conventional identification-estimation scheme such as multiple-model adaptive estimators (MMAEs) or interacting multiple-models (IMMs), is discarded. To increase the training speed and identification accuracy, the improved multiple-model mechanism (IMMM) is adopted, and a multiple-model layer, in which regimes representing different values are set, is connected behind a conventional neural network. Since the navigation ratios are identified online, the connections between missiles are decoupled, and only one filter is required for each missile. This could greatly reduce the computational burden of onboard computers. The effectiveness of the proposed online identification model and the performance of the state estimation filter are demonstrated through numerical simulations.
AB - An online navigation ratio identification model based on the gated recurrent unit (GRU) and a state estimation extended Kalman filter (EKF) are proposed under the scenario in which multiple enemy missiles attack a stationary target using a time-cooperative guidance law. The navigation ratio identification is solved as a dynamic problem, and the time-varying navigation ratios of each missile, instead of the effective navigation constants and cooperative gains, are identified in this paper. In other words, the simplified assumption that the true value is within a known finite set, which is generally adopted in a conventional identification-estimation scheme such as multiple-model adaptive estimators (MMAEs) or interacting multiple-models (IMMs), is discarded. To increase the training speed and identification accuracy, the improved multiple-model mechanism (IMMM) is adopted, and a multiple-model layer, in which regimes representing different values are set, is connected behind a conventional neural network. Since the navigation ratios are identified online, the connections between missiles are decoupled, and only one filter is required for each missile. This could greatly reduce the computational burden of onboard computers. The effectiveness of the proposed online identification model and the performance of the state estimation filter are demonstrated through numerical simulations.
KW - Artificial neural network
KW - Gated recurrent units
KW - Improved multiple model mechanism
KW - Parameter identification
UR - http://www.scopus.com/inward/record.url?scp=85150441674&partnerID=8YFLogxK
U2 - 10.1016/j.ast.2023.108261
DO - 10.1016/j.ast.2023.108261
M3 - Article
AN - SCOPUS:85150441674
SN - 1270-9638
VL - 136
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 108261
ER -