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

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 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 …

In this paper, a cooperative guidance law is proposed for missiles with thrust control to
realize impact angle constrained salvo attack, where missile speed limit is also considered …

Abstract The problem of Impact Time Control Guidance (ITCG) with field-of-view (FOV)
constraint is investigated. The proposed ITCG law is a combination of the well-known …

MAINTAINING seeker lock on to the target is critical for the success of any missile
engagement. Imposing a terminal impact angle constraint may result in curved missile …

The problem of distributed cooperative guidance with arbitrary impact angle constraint is
addressed. A new distributed cooperative guidance law, which consists of a local control …

Nomenclature a= missile lateral acceleration, m∕ s2 amax= limit of missile lateral
acceleration, m∕ s2 N= proportional-navigation gain r= range between missile and target …

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 …