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Avtomatika i Telemekhanika, 2021, Issue 9, Pages 73–85
DOI: https://doi.org/10.31857/S0005231021090026 (Mi at15621) 		 
This article is cited in 1 scientific paper (total in 1 paper)

Linear Systems

Methods for aircraft guidance with changes in control priorities

V. S. Verba

JSC Radio-Engineering Corporation “Vega”, Moscow, 121170 Russia
Full-text PDF (210 kB) Citations (1)
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DOI: https://doi.org/10.31857/S0005231021090026
Abstract: We consider various possible implementations of changes in control priorities in aircraft guidance based on time-varying state models, variable penalty coefficients in performance functionals, and allowance for the discrepancy between the interceptor and target dynamic properties. For each possible implementation, specific examples of the guidance method synthesis are given and analyzed.
Keywords: change in control priorities, local optimization of guidance systems, time-varying self-guidance method.
Funding agency Grant number
Russian Foundation for Basic Research 18-08-01083_а
This work was financially supported by the Russian Foundation for Basic Research, project no. 19-08-00060-a.
Presented by the member of Editorial Board: R. A. Munasypov

Received: 08.12.2020
Revised: 22.04.2021
Accepted: 29.04.2021
English version:
Automation and Remote Control, 2021, Volume 82, Issue 9, Pages 1519–1529
DOI: https://doi.org/10.1134/S0005117921090022
Bibliographic databases:
Document Type: Article
Language: Russian
Citation: V. S. Verba, “Methods for aircraft guidance with changes in control priorities”, Avtomat. i Telemekh., 2021, no. 9, 73–85; Autom. Remote Control, 82:9 (2021), 1519–1529
Citation in format AMSBIB
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  • https://www.mathnet.ru/eng/at/y2021/i9/p73
    • This publication is cited in the following 1 articles:
    Citing articles in Google Scholar: Russian citations, English citations
    Related articles in Google Scholar: Russian articles, English articles
    		Avtomatika i Telemekhanika
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    Abstract page:155
    Full-text PDF :6
    References:43
    First page:34
     
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