This paper proposes a novel three-dimensional (3D) intelligent impact time control guidance
(ITCG) law with the field-of-view (FOV) strictly constrained based on nonlinear relative …

MISSILE guidance laws are designed primarily to achieve zero miss distance. However, in
the context of modern warfare, conventional guidance laws have limitations in the face of a …

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 an impact angle control guidance law that confines the missile look
angle during homing in order to not exceed a seeker's field-of-view limit. A sliding surface …

In this paper, we propose a guidance law that considers the field-of-view (FOV) limitation as
well as the impact angle and time constraints. In order to develop the guidance law, we first …

This paper proposes a guidance law that achieves the desired terminal impact time without
violating a seeker's field-of-view (FOV) limits. In order to derive the guidance law, kinematic …

This article proposes a guidance strategy that enables the interceptor to control its impact
time against stationary targets, while also meeting the field-of-view (FOV) constraints of the …

Most existing impact angle control guidance (IACG) laws that consider the reduced seeker
field-of-view (FOV) focus only on a stationary or a nonmaneuvering moving target. In actual …

TO EFFECTIVELY saturate the enemy's defense system, control of the time of interception is
important [1]. Homing interceptors use their own seekers to locate and pursue targets …

To effectively control impact time and ensure terminal acceleration converges to zero under
the look angle constraint, this paper proposes a generalized circular impact time guidance …