Simultaneous attack strategy against a maneuvering target with unknown acceleration-Reference-Cited by-同舟云学术

Simultaneous attack strategy against a maneuvering target with unknown acceleration

Published:2017-08-31 Issue:1 Volume:233 Page:71-80
ISSN:0954-4100
Container-title:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
language:en
Short-container-title:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Author:

Hu Zilun¹,Yang Jianying¹

Affiliation:

1. The State Key Laboratory for Turbulence and Complex Systems, Department of Mechanics and Engineering Science, College of Engineering, Peking University, Beijing, PR China

Abstract

This paper is concerning the simultaneous attack problem with multiple missiles against a maneuvering target with unknown acceleration. The new guidance protocol, which avoids using the time-to-go information, ensures the simultaneous attack based on the consensus of the range-to-go and the approaching rate of each missile. This strategy is a distributed guidance law where each missile can only get information from neighbors. The consensus of the missiles is shown mathematically as well as with extensive simulations.

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

Link

http://journals.sagepub.com/doi/pdf/10.1177/0954410017727026

Reference14 articles.

1. Cooperative Optimal Guidance Laws for Imposing a Relative Intercept Angle

2. Consensus Tracking of Multi-Agent Systems With Lipschitz-Type Node Dynamics and Switching Topologies

3. Cooperative Strategies for Optimal Aircraft Defense from an Attacking Missile

4. Accurate Time-to-Go Estimation for Proportional Navigation Guidance

5. Guidance law to control impact time and angle

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