In this article, fixed-time cooperative guidance laws are designed for multiple missiles to
simultaneously attack a maneuvering target at desired terminal angles. The 3-D guidance …

This paper proposes distributed cooperative guidance laws for multiple missiles with
constant speeds to achieve impact-angle-constrained salvo attack against a stationary target …

This article proposes a leader-follower cooperative salvo guidance strategy to intercept
nonmaneuvering targets by exploiting the advantages of supertwisting sliding mode control …

In this paper, a cooperative guidance law is proposed for missiles with thrust control to
realize impact angle constrained salvo attack, where missile speed limit is also considered …

THE primary objective of missile guidance laws is to drive the missile to intercept a specific
target with zero miss distance. Proportional navigation guidance (PNG) has been proven to …

In this paper, a distributed three-dimensional (3D) nonsingular cooperative guidance law is
designed for multiple missiles with different seeker's field-of-view (FOV) constraints to …

RECENT years have witnessed a rapid development on cooperative homing guidance of
multiple missiles. In essence, cooperative homing guidance aims to achieve the salvo attack …

COOPERATIVE guidance of multiple vehicles for simultaneous arrival is an effective way to
increase the success rate of, for example, missile–target interception. The seminal research …

This paper investigates the problem of impact-time-control and proposes a learning-based
computational guidance algorithm to solve this problem. The proposed guidance algorithm …

This paper presents a new guidance strategy for a certain class of homing missiles subject
to various terminal constraints and lateral acceleration limit. To achieve zero miss distance …