2021
DOI: 10.1109/access.2021.3049571
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A Novel Cooperative Control System of Multi-Missile Formation Under Uncontrollable Speed

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Cited by 8 publications
(5 citation statements)
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“…The trajectories of the two situations are shown in Figures 5 and 6, and the corresponding analytical results are presented in Figures 7 and 8. It can be observed that the convergent resultant error was maintained in a small interval (within 0.05) in both cases, and the results were of comparable if not better accuracy than the comparison results in [33], which kept the position error within 50 m. In addition, good synchronization of the speed and heading angles among the missiles was achieved, although the neighboring speed information was not provided.…”
Section: Basic Formation Controlmentioning
confidence: 74%
See 1 more Smart Citation
“…The trajectories of the two situations are shown in Figures 5 and 6, and the corresponding analytical results are presented in Figures 7 and 8. It can be observed that the convergent resultant error was maintained in a small interval (within 0.05) in both cases, and the results were of comparable if not better accuracy than the comparison results in [33], which kept the position error within 50 m. In addition, good synchronization of the speed and heading angles among the missiles was achieved, although the neighboring speed information was not provided.…”
Section: Basic Formation Controlmentioning
confidence: 74%
“…First, we incorporate a policy constraint approach to enhance the stability of the algorithm in order to optimize the objective function and find the Nash equilibrium strategy. The proposed algorithm is more flexible for adapting to varying control objectives compared with conventional approaches [4,[31][32][33]. Then, an adaptive topology scheme is designed to address the common node failure problem in formation control, and this method can achieve stable communication connections at a relatively low communication cost.…”
Section: Introductionmentioning
confidence: 99%
“…However, since the information of missile guidance control system is transmitted via wireless channel, there will have some undesired effects during the information transmission, e.g., data dropout (packet drop) and network-induced delay. On the other hand, different than the conventional single missile system, the multi-missile system is a popular issue and it has been widely addressed by researchers in recent years [49]- [51]. In this situation, to achieve more difficult missions, a set of missile systems are controlled to maintain the desired formation during the maneuvering process.…”
Section: Discussionmentioning
confidence: 99%
“…The above LMIs-constrained optimization problem is also called eigenvalue problem (EVP) and can be solved very efficiently by convex optimization algorithm [48]. More specifically, this problem can be solved by decreasing ρ 2 until W 1 > 0 and P 2 > 0 cannot be found in (40) and (49).…”
Section: Proof See Appendix Bmentioning
confidence: 99%
“…They introduced a proposed abstraction of an aerial swarm system architecture to help developers to understand the main required modules. Zhang et al [13] investigated a novel cooperative control system based on the sliding mode variable structure control theory for multimissile formation flight. According to numerical simulations, the method proposed in this article could achieve similar relative position errors under the condition of uncontrollable speed.…”
Section: Introductionmentioning
confidence: 99%