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 …

INTERCEPTOR guidance laws are designed to satisfy the primary requirement of driving to
zero the closing distance to the target. However, many practical engagements impose …

In this paper, a new guidance strategy is proposed for intercepting stationary and constant-
velocity moving targets with desired impact time and angle via a virtual target approach …

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 …

The problem of salvo attack of multiple missiles without time-to-go estimation has been
addressed by a two-stage guidance scheme in this correspondence. In the first stage, a …

WHEN a pursuer for some reason modifies its otherwise direct course toward a target, two
key quantities that become significantly influenced are the impact time and the impact angle …

In this paper, an impact time and angle constrained guidance (ITACG) is proposed based on
the nonsingular terminal sliding mode control (NTSMC) theory. First, the guidance law is …

This paper is concerned with devising nonlinear optimal guidance for intercepting a
stationary target with a desired impact time. According to Pontryagin's maximum principle …

COOPERATIVE attack of multiple missiles is known as a countermeasure to cope with
defensive targets such as modern warships [1]. In this strategy, multiple missiles are …

Abstract In Jeon et al.(2010), a cooperative PNG (Proportional Navigation Guidance) law
was proposed to achieve the salvo attack using multiple missiles. When the leading angle is …