https://orcid.org/0000-0002-2626-8617
https://orcid.org/0000-0003-0136-0174
https://orcid.org/0000-0001-9044-7137
https://orcid.org/0000-0002-2626-8617
https://orcid.org/0000-0003-0136-0174
https://orcid.org/0000-0001-9044-7137
A critical challenge in missile guidance is the frequent inaccessibility of essential target information by on-board seekers. This article studies the 3-D cooperative guidance issue of multiple missiles simultaneously attacking an unknown maneuvering target. Different from most existing research, the pitch and yaw lead angles of a maneuvering target are entirely unknown, while the position and velocity information is only accessible to neighboring missiles. An adaptive distributed estimator is designed to estimate the target information over a directed communication network, generating a transmitted target with similar maneuverability to the actual target for each missile. Boundedness of the estimation errors are guaranteed within a prescribed time. Subsequently, a modified guidance law that integrates proportional navigation and coordination components is developed for simultaneously tracking the trajectories of the transmitted targets. The superiority of the developed adaptive cooperative estimation and guidance approach is confirmed through simulations.
Adaptive Cooperative Estimation and Guidance Against Unknown Maneuvering Target
IEEE Transactions on Aerospace and Electronic Systems ; 61 , 4 ; 9129-9140
2025-08-01
2827293 byte
Article (Journal)
Electronic Resource
English
Fixed-Time Convergence Cooperative Guidance Law Against Maneuvering Target
| British Library Conference Proceedings | 2022
Fixed-Time Convergence Cooperative Guidance Law Against Maneuvering Target
| Springer Verlag | 2021
Guidance Law Design Against Unknown Maneuvering Target Based on Two ESOs
| Springer Verlag | 2023