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 paper aims to examine the potential of using the emerging deep reinforcement learning
techniques in missile guidance applications. To this end, a Markovian decision process that …

This paper investigates the problem of impact-angle-constrained guidance law design
against maneuvering target with large initial heading error. The guidance problem is first …

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 …

FOR decades, the proportional navigation guidance (PNG) law has been widely applied in
various guidance problems due to its implementation simplicity and efficiency [1]. The PNG …

This paper proposes a varying-gain proportional navigation guidance (PNG) law that can
serve as the baseline for precise control of impact time. First, a varying-gain PNG law is …

Considering an air-based missile intercepting maneuvering target with desired impact
angles, robust guidance laws with autopilot lag in three-dimensional coupling space are …

Abstract The three-dimensional (3D) impact time and angle guidance problem is of great
practical significance but remains open because of the coupling nonlinearity and multiple …