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, two kinds of sliding-mode guidance laws with impact time constraint are
proposed for intercepting various target motions, including nonmaneuvering and …

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

THE primary objective of missile guidance laws is to drive the missile to intercept a specific
target with zero miss distance. Proportional navigation guidance (PNG) has been proven to …

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 …

In this paper, a novel cooperative guidance law is proposed to make multiple missiles in the
three-dimensional (3-D) space hit simultaneously the same target at pre-specified impact …

This paper proposes a varying-gain proportional navigation guidance (PNG) law that can
serve as the baseline for precise control of impact time. First, a varying-gain PNG law is …

This paper proposes a three-dimensional, nonlinear guidance strategy for terminal-time-
constrained interception of a nonmaneuvering target. The restrictive assumption of …

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 …