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Predefined-time prescribed performance guidance law design against maneuvering target under input saturation

  • CAS - Institute of Mechanics
  • School of Astronautics, Harbin Institute of Technology

Research output: Contribution to journalConference articlepeer-review

Abstract

A novel SMC-based prescribed performance guidance law combined with a base generator (TBG) is proposed. A TBG-based modified Lyapunov function is first proposed, which ensures that the LOS tracking error converges into zero within a predefined time. A novel sliding manifold with adjusting convergent time property is proposed, which brings about a smaller control magnitude and predefined time convergent rate. To ensure a satisfied transit and steady performance, some converted variables are defined based on which a novel prescribed performance guidance law is constructed. The input saturation problem is properly solved by designing a novel TBG-based one-order auxiliary system. Extensive simulation results have verified the effectiveness of the proposed method.

Original languageEnglish
Article number012083
JournalJournal of Physics: Conference Series
Volume2764
Issue number1
DOIs
StatePublished - 2024
Externally publishedYes
Event2023 2nd International Conference on Aerospace and Control Engineering, ICoACE 2023 - Nanjing, China
Duration: 15 Dec 202317 Dec 2023

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