The unique performance advantages of hypersonic vehicles represent a critical challenge
for existing defense systems. To facilitate defensive operations against hypersonic vehicles …

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

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 …

An impact-time-control guidance (ITCG) law is required for simultaneous attack of multiple
missiles. In application of ITCG, the limit of seeker look angle should be regarded as an …

In this paper, an impact angle control guidance law, which considers simultaneously the
impact angle and seeker's look angle constraints, is proposed for a constant speed missile …

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 …

This paper investigates one integrated guidance and control (IGC) method for missiles with
strapdown seeker. The IGC model considering the field-of-view (FOV) constraint is built by …

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 …

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 …

A biased proportional navigation guidance law, considering the seeker's look angle and
acceleration capability limits, for impact-angle-control against nonmaneuvering targets is …