For the three-dimensional terminal guidance problem of multiple missiles cooperatively
intercepting a maneuvering target, a novel finite-time cooperative guidance law with impact …

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 …

In this paper, sliding mode control-based impact time guidance laws are proposed. Even for
large heading angle errors and negative initial closing speeds, the desired impact time is …

This article proposes a leader-follower cooperative salvo guidance strategy to intercept
nonmaneuvering targets by exploiting the advantages of supertwisting sliding mode control …

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 …

This paper presents the unified cooperative strategies for the salvo attack of multiple
missiles on the basis of the traditional proportional navigation (PN) algorithm. The …

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 …

This paper presents the cooperative strategies for salvo attack of multiple missiles based on
the classical proportional navigation (PN) algorithm. The three-dimensional (3-D) guidance …

In this paper, the sliding mode control based guidance laws to intercept stationary targets at
a desired impact time are proposed. Then, it is extended to constant velocity targets using …

COOPERATIVE guidance of multiple vehicles for simultaneous arrival is an effective way to
increase the success rate of, for example, missile–target interception. The seminal research …