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 …

Cooperative guidance issues with impact time consensus against a maneuvering target are
considered in this article. Different from the existing achievements, the expected impact time …

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 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 …

In order to improve the flexibility and reduce the energy consumption of cooperative
guidance laws considering the impact angle constraint, this paper proposes a three …

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 …

This article presents a nonlinear 3-D guidance law for homing missiles with a field-of-view
(FOV) constraint to achieve impact time and angle control against a stationary target …

This paper investigates the three-dimensional (3D) spatial–temporal cooperative guidance
problem for multiple missiles with time-varying speeds, which is addressed by a progressive …

To address the problem wherein multiple missiles attack a target simultaneously in a three-
dimensional space at an adjustable impact time and expected impact angles, this paper …

TRADITIONAL guidance laws like classical proportional navi-gation guidance (PNG) usually
only focus on zero miss distance. However, with the rapid growth of modern defense system …