Guidance laws based on a conventional sliding mode ensures only asymptotic
convergence. However, convergence to the desired impact angle within a finite time is …

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

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 …

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 …

The nonlinear impact angle control problem of a physically constrained pursuer against a
stationary ground target is solved through the use of a two-phased proportional navigation …

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 …

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 investigates the three-dimensional (3-D) interception guidance problem, where
the missile is required to intercept the maneuvering target with the desired terminal angles …

In this paper, an impact angle control guidance (IACG) law with predefined convergence
time and seeker's field-of-view (FOV) limit is proposed in three-dimensional (3D) scenario …