Abstract
In this paper,we propose a cooperative guidance law aimed to achieve coordinated impact angles with limited observation on target information.The primary challenge lies in estab-lishing an appropriate communication graph among all missiles and devising an algorithm to esti-mate target acceleration information during engagements.To address this,we propose a specific communication topology and employ a numerical integration-based estimation method.Addition-ally,a distributed algorithm is introduced to facilitate consensus on target acceleration estimation.Building upon these foundations,we design an optimal-control-based distributed guidance law for each missile.Performance of the proposed guidance law is validated through numerical simulations.
基金项目
NSFC(62088101)
Zhejiang Provincial Natural Science Foundation of China(LR20F030003)
NETL
NSTL
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