For the terminal guidance problem of missiles intercepting maneuvering targets in the three-
dimensional space, the design of guidance laws for non-decoupling three-dimensional …

PROPORTIONAL navigation (PN) and its variants have been widely used as homing
guidance laws because they are highly efficient and easy for implementation [1–10]. The PN …

The problem of missile interception is investigated in this paper. Sliding-mode controllers
with finite-time convergence are proposed for the design of guidance laws. In particular, the …

By considering the dynamics of a missileʼs autopilot as a first-order lag, a guidance law with
finite time convergence is designed based on target–missile relative motion equations. It is …

In this paper, a model-predictive-control (MPC)-based cooperative guidance law is
presented to perform a salvo attack against a stationary target, which guarantees 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 …

A new adaptive nonlinear guidance law is proposed here. The fourth order state equation for
integrated guidance and control loop is formulated taking into consideration the target …

The terminal guidance problem for missiles intercepting maneuvering targets with terminal
impact angle constraints is investigated. Regarding the target acceleration as an unknown …

This paper considers the terminal guidance problem of missiles intercepting maneuvering
targets with impact angle constraints. Based on an advanced nonsingular fast terminal …

DURING the past several decades, a large number of methods have been designed to solve
guidance problems, ranging from proportional navigation (PN) to robust control algorithms …