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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Veröffentlicht in:	Transactions of Nanjing University of Aeronautics & Astronautics Jg. 42; H. 4; S. 541 - 553
Hauptverfasser:	Li, Guilin, Zhou, Wei, Zhang, Jiaru
Format:	Journal Article
Sprache:	Chinesisch Englisch
Veröffentlicht:	Nanjing Nanjing University of Aeronautics and Astronautics 01.08.2025 Editorial Office of Transactions of Nanjing University of Aeronautics and Astronautics
Schlagworte:	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-Zugang:	Volltext
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