Finite-Time Distributed Cooperative Guidance Law with Impact Angle Constraint

The problem of the distributed cooperative guidance law of multiple missiles attacking a stationary target with impact angle constraint is investigated. A distributed cooperative guidance law, which consists of a nonsingular terminal sliding mode component for ensuring finite time convergence to the...

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Main Authors: Wenguang Zhang, Jin Yan
Format: Article
Language:English
Published: Wiley 2023-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2023/5568394
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author Wenguang Zhang
Jin Yan
author_facet Wenguang Zhang
Jin Yan
author_sort Wenguang Zhang
collection DOAJ
description The problem of the distributed cooperative guidance law of multiple missiles attacking a stationary target with impact angle constraint is investigated. A distributed cooperative guidance law, which consists of a nonsingular terminal sliding mode component for ensuring finite time convergence to the desired LOS angle and a coordination component for realizing finite time consensus of time-to-go estimates, is proposed. Analysis shows that the guidance law designed in this study can ensure that missiles’ time-to-go estimates represent real times to go once all the missiles fly along the desired LOS. Therefore, simultaneous arrival can be guaranteed. Furthermore, it is modified to accommodate the communication failure cases. Compared with existing results, this guidance law owns faster convergence rate and can satisfy large impact angles. Numerical simulations are performed to demonstrate the effectiveness of the proposed guidance law.
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institution DOAJ
issn 1687-5974
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publishDate 2023-01-01
publisher Wiley
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series International Journal of Aerospace Engineering
spelling doaj-art-33ececce512046e5aaeef0fdabfeefe52025-08-20T03:18:34ZengWileyInternational Journal of Aerospace Engineering1687-59742023-01-01202310.1155/2023/5568394Finite-Time Distributed Cooperative Guidance Law with Impact Angle ConstraintWenguang Zhang0Jin Yan1School of Information EngineeringSchool of Computer Science and EngineeringThe problem of the distributed cooperative guidance law of multiple missiles attacking a stationary target with impact angle constraint is investigated. A distributed cooperative guidance law, which consists of a nonsingular terminal sliding mode component for ensuring finite time convergence to the desired LOS angle and a coordination component for realizing finite time consensus of time-to-go estimates, is proposed. Analysis shows that the guidance law designed in this study can ensure that missiles’ time-to-go estimates represent real times to go once all the missiles fly along the desired LOS. Therefore, simultaneous arrival can be guaranteed. Furthermore, it is modified to accommodate the communication failure cases. Compared with existing results, this guidance law owns faster convergence rate and can satisfy large impact angles. Numerical simulations are performed to demonstrate the effectiveness of the proposed guidance law.http://dx.doi.org/10.1155/2023/5568394
spellingShingle Wenguang Zhang
Jin Yan
Finite-Time Distributed Cooperative Guidance Law with Impact Angle Constraint
International Journal of Aerospace Engineering
title Finite-Time Distributed Cooperative Guidance Law with Impact Angle Constraint
title_full Finite-Time Distributed Cooperative Guidance Law with Impact Angle Constraint
title_fullStr Finite-Time Distributed Cooperative Guidance Law with Impact Angle Constraint
title_full_unstemmed Finite-Time Distributed Cooperative Guidance Law with Impact Angle Constraint
title_short Finite-Time Distributed Cooperative Guidance Law with Impact Angle Constraint
title_sort finite time distributed cooperative guidance law with impact angle constraint
url http://dx.doi.org/10.1155/2023/5568394
work_keys_str_mv AT wenguangzhang finitetimedistributedcooperativeguidancelawwithimpactangleconstraint
AT jinyan finitetimedistributedcooperativeguidancelawwithimpactangleconstraint