A composite formation strategy for multiple missiles

Wang, Xiaofang; Liu, Dong‐Ze; Tian, Zhen

doi:10.1109/iccar.2017.7942784

Cited by 5 publications

(3 citation statements)

References 10 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…Many scholars used an autopilot to design the formation controller. Wang et al considered multiple constraints such as the initial position, the end position and collision avoidance, and designed an optimal trajectory based on the Gaussian pseudo-spectrum method [12]. [13][14][15] all used an autopilot for formation controller design.…”

Section: B Literature Reviewmentioning

confidence: 99%

See 1 more Smart Citation

A Novel Cooperative Control System of Multi-Missile Formation Under Uncontrollable Speed

Zhang

Han

2021

IEEE Access

View full text Add to dashboard Cite

Section: B Literature Reviewmentioning

confidence: 99%

“…Substituting the above matrices into (12), the further simplified model of the formation control problem can be obtained:…”

Section: B Formation Problem Modelmentioning

confidence: 99%

A Novel Cooperative Control System of Multi-Missile Formation Under Uncontrollable Speed

Zhang

Han

2021

IEEE Access

View full text Add to dashboard Cite

“…The dynamic surface controllers were introduced for solving the formation tracking issues for multiple missiles system in Ref. (16). In Ref.…”

Section: Introductionmentioning

confidence: 99%

Adaptive sliding mode formation control for multiple flight vehicles with considering autopilot dynamic

Li¹,

Qin²,

Zhou³

2021

Aeronaut. j.

View full text Add to dashboard Cite

This paper mainly focuses on the cooperative control of formation configuration for multiple flight vehicles in the three-dimensional space. Considering the external disturbance of the system, the adaptive non-singular terminal sliding mode control law (NTSMC) is designed based on the virtual leader-follower method, which aims to ensure that each flight vehicle reaches the expected terminal position in a limited time and meet the configuration constraints. Further considering the first-order dynamic characteristic of the autopilot, a novel second-order sliding mode control (SOSMC) law is deduced with using the estimated information of sliding mode disturbance observer. The proposed control method ensures that all flight vehicles form the required space formation configuration simultaneously at a pre-designed time, and the chattering phenomenon of the sliding mode surface and acceleration response that nears the equilibrium point is effectively weaken. The stability of the proposed control law is verified by theoretical analysis and lots of mathematical simulations. The results show that the control algorithm in this paper can be used to guidance the formation controller design of multiple flight vehicles in the mid-guidance phase to some extent, and thus the cooperative flight stability of the system can be effectively improved.

show abstract