Anti-acceleration Saturation Terminal Guidance Law Based on LSTM

Missile acceleration saturation in a practical terminal guidance process may significantly reduce the interception performance. To solve this problem, this paper presents an anti-saturation guidance law with finite-time convergence for a three dimensional maneuvering interception. The finite time bo...

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Bibliographic Details

Published in:	Transactions of Nanjing University of Aeronautics & Astronautics Vol. 42; no. 4; pp. 541 - 553
Main Authors:	Li, Guilin, Zhou, Wei, Zhang, Jiaru
Format:	Journal Article
Language:	Chinese English
Published:	Nanjing Nanjing University of Aeronautics and Astronautics 01.08.2025 Editorial Office of Transactions of Nanjing University of Aeronautics and Astronautics
Subjects:	anti-acceleration saturation finite-time boundedness （ftb） input-output finite time stability （io-fts） Jamming performance long short-term memory network （lstm） Maneuvering targets Missile control Missile tracking Nonlinear systems Terminal guidance terminal guidance law Tracking
ISSN:	1005-1120
Online Access:	Get full text
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