Air-breathing hypersonic vehicle has great military and potential economic value due to its
characteristics: high velocity, long range, quick response. Therefore, the development of …

A new guidance law with both impact time and impact angle constraints is proposed in this
paper. We first simplify missile dynamics under small heading error approximation, and …

THE well-justified proportional navigation guidance (PNG) law [1, 2] and its variants have
been widely used in missile guidance during the last few decades. The long history of …

This paper proposes a coverage-based cooperative guidance (CBCG) law to enable low-
velocity and constrained-manoeuvrability interceptors to intercept a hypersonic vehicle …

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 proposes a new three-dimensional optimal guidance law for impact time control
with seeker's Field-of-View (FOV) constraint to intercept a stationary target. The proposed …

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 …

This paper develops a new class of distributed cooperative guidance laws under both
undirected and directed communication topologies based on the circular guidance and the …

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 …

In order to improve the multiple-missile cooperative attack capability and penetration
capability, this paper investigates two three-dimensional impact-angle-constrained …