Consensus-Based Two-Stage Salvo Attack Guidance

He, Shaoming; Wei, Wang; Lin, Defu; Lei, Hong-Bo

doi:10.1109/taes.2017.2773272

Cited by 83 publications

(22 citation statements)

References 24 publications

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“…Theorem 2. Considering a group of n missiles guided by BPNG law, and they subjected to communication graph G and the kinematics equations (4) and (5), the simultaneous attack can be achieved by the proposed distributed consensus protocol (32).…”

Section: The Consensus Protocol Of Simultaneous Attackmentioning

confidence: 99%

“…An alternative countermeasure which can facilitate missile attacker surviving the threats of the defense systems is to conduct a simultaneous attack with multiple missiles coming from different directions. [1][2][3][4][5][6] Obviously, it is difficult to defend against a group of incoming missile attackers cropping up at the same time along different directions, even though the attackers are conventional ones in performance. 1,3 In view of the abovementioned facts, cooperative attack of multiple missiles has been considered as an effective countermeasure to improve missile's penetration probability, and it has been an active and attractive research topic.…”

Section: Introductionmentioning

confidence: 99%

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Distributed target-encirclement guidance law for cooperative attack of multiple missiles

Yan

Fan

Liu

et al. 2020

International Journal of Advanced Robotic Systems

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The target-encirclement guidance problem for many-to-one missile-target engagement scenario is studied, where the missiles evenly distribute on a target-centered circle during the homing guidance. The proposed distributed target-encirclement guidance law can achieve simultaneous attack of multiple missiles in different line-of-sight directions. Firstly, the decentralization protocols of desired line-of-sight angles are constructed based on the information of neighboring missiles. Secondly, a biased proportional navigation guidance law that can arbitrarily designate the impact angle is cited. The missiles can achieve all-aspect attack on the target in an encirclement manner by combining the biased proportional navigation guidance law and dynamic virtual targets strategy. Thirdly, the consensus protocol of simultaneous attack is designed, which can guarantee that all missiles’ time-to-go estimates achieve consensus asymptotically, and the convergence of the closed-loop system is proved strictly via the Lyapunov stability theory. Finally, numerical simulation results demonstrate the performance and feasibility of the proposed distributed target-encirclement guidance law in different engagement situations.

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Section: The Consensus Protocol Of Simultaneous Attackmentioning

confidence: 99%

Section: Introductionmentioning

confidence: 99%

Distributed target-encirclement guidance law for cooperative attack of multiple missiles

Yan

Fan

Liu

et al. 2020

International Journal of Advanced Robotic Systems

View full text Add to dashboard Cite

show abstract

“…For this reason, we first perform simulations with various guidance gains K = 4, 8, 12. In these simulations, the desired impact time is set as t d = 45s, which satisfies condition (25). The simulation results, including interception trajectories, history of relative range and acceleration command, are presented in Fig.…”

Section: A Characteristics Of the Proposed Three-dimensional Impact mentioning

confidence: 99%

Three-Dimensional Optimal Impact Time Guidance for Antiship Missiles

Lin

2019

Journal of Guidance, Control, and Dynamics

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“…The first term of equation (10) is the PPNG law, and the second is the PG law. PPNG and PG laws are widely used in missile community due to their easy implementation and effectiveness [26]. PPNG keeps a constant LOS angle, and PG directs a missile along the LOS [27].…”

Section: Design Of Guidance Lawmentioning

confidence: 99%

A Three-Dimensional Guidance Logic for Continuous Curvature Path Following

Park

2019

International Journal of Aerospace Engineering

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A new simple and practical guidance logic is proposed for a vehicle to follow a general continuous curvature path defined in a three-dimensional space. The proposed guidance logic is formulated in such a way that the guidance law is to generate the command acceleration such that a vehicle pursues the designed moving virtual target, and this eventually makes a vehicle to follow a desired path. The position and velocity of the virtual target are specified explicitly by introducing the concept of the projection point and the tangentially receding distance. Numerical simulations are conducted to evaluate the precise path-following capability of the proposed guidance logic.

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Consensus-Based Two-Stage Salvo Attack Guidance

Cited by 83 publications

References 24 publications

Distributed target-encirclement guidance law for cooperative attack of multiple missiles

Distributed target-encirclement guidance law for cooperative attack of multiple missiles

Three-Dimensional Optimal Impact Time Guidance for Antiship Missiles

A Three-Dimensional Guidance Logic for Continuous Curvature Path Following

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