This article investigates the simultaneous attack problem of multiple missiles against a manoeuvring target with delayed information transmission in three-dimensional space. Based on the kinetic model of the missiles, the problem is divided into three demands: the velocity components normal to line-of-sight converge to zero in finite time, the component of motion states along line-of-sight should achieve consensus and converge to zero. The guidance law is designed for each demand and by theoretical proof, the upper bound of delay which can tolerate is presented and the consensus error of the relative distances can converge to a small neighbourhood of zero. And simulation example presented also demonstrates the validity of the theoretical re...
The consensus problem of impact time is addressed for multiple anti-ship missiles. A new distributed...
Aiming at the problem that multiple Unmanned Aerial Vehicles (UAVs) attack the stationary target coo...
A new cooperative guidance law based on terminal sliding mode with strengthened condition is designe...
The target-encirclement guidance problem for many-to-one missile-target engagement scenario is studi...
summary:In this paper, a new guidance problem with the impact time constraint for cooperative attack...
AbstractThis paper presents the cooperative strategies for salvo attack of multiple missiles based o...
This paper considers the simultaneous attack problem of multiple missiles against a stationary targe...
This paper considers the simultaneous attack problem of multiple missiles against a stationary targe...
The cooperative simultaneous attack problem with multiple missiles against a single target under lea...
This paper concerns on the simultaneous attack problem with multiple missiles against a maneuvering ...
AbstractThe consensus problem of impact time is addressed for multiple anti-ship missiles. A new dis...
Introduction: The primary objective of missile guidance laws is to drive the missile to intercept a ...
A new nonlinear guidance law for air-to-ground missile cooperation attacks is proposed in this paper...
Most publications discussing missile interception systems assume a zero computer response time. This...
AbstractCooperative guidance problems of multiple missiles are considered in this article. A coopera...
The consensus problem of impact time is addressed for multiple anti-ship missiles. A new distributed...
Aiming at the problem that multiple Unmanned Aerial Vehicles (UAVs) attack the stationary target coo...
A new cooperative guidance law based on terminal sliding mode with strengthened condition is designe...
The target-encirclement guidance problem for many-to-one missile-target engagement scenario is studi...
summary:In this paper, a new guidance problem with the impact time constraint for cooperative attack...
AbstractThis paper presents the cooperative strategies for salvo attack of multiple missiles based o...
This paper considers the simultaneous attack problem of multiple missiles against a stationary targe...
This paper considers the simultaneous attack problem of multiple missiles against a stationary targe...
The cooperative simultaneous attack problem with multiple missiles against a single target under lea...
This paper concerns on the simultaneous attack problem with multiple missiles against a maneuvering ...
AbstractThe consensus problem of impact time is addressed for multiple anti-ship missiles. A new dis...
Introduction: The primary objective of missile guidance laws is to drive the missile to intercept a ...
A new nonlinear guidance law for air-to-ground missile cooperation attacks is proposed in this paper...
Most publications discussing missile interception systems assume a zero computer response time. This...
AbstractCooperative guidance problems of multiple missiles are considered in this article. A coopera...
The consensus problem of impact time is addressed for multiple anti-ship missiles. A new distributed...
Aiming at the problem that multiple Unmanned Aerial Vehicles (UAVs) attack the stationary target coo...
A new cooperative guidance law based on terminal sliding mode with strengthened condition is designe...