An Autonomous Attack Guidance Method with High Aiming Precision for UCAV Based on Adaptive Fuzzy Control under Model Predictive Control Framework

被引:7
|
作者
Yang, Zhen [1 ]
Sun, Zhixiao [2 ]
Piao, Haiyin [1 ]
Zhao, Yiyang [1 ]
Zhou, Deyun [1 ]
Kong, Weiren [1 ]
Zhang, Kai [1 ]
机构
[1] Northwestern Polytech Univ, Sch Elect & Informat, Xian 710072, Peoples R China
[2] Northwestern Polytech Univ, Unmanned Syst Res Inst, Xian 710072, Peoples R China
来源
APPLIED SCIENCES-BASEL | 2020年 / 10卷 / 16期
基金
中国国家自然科学基金;
关键词
UCAV; beyond-visual-range (BVR) air combat; autonomous attack guidance; model predictive control (MPC); adaptive fuzzy guidance controller; MANEUVER STRATEGY; CONTROL ALGORITHM; FIGHTER; DESIGN; SYSTEM;
D O I
10.3390/app10165677
中图分类号
O6 [化学];
学科分类号
0703 ;
摘要
With its superior performance, the unmanned combat air vehicle (UCAV) will gradually become an important combat force in the future beyond-visual-range (BVR) air combat. For the problem of UCAV using the BVR air-to-air missile (AAM) to intercept the highly maneuvering aerial target, an autonomous attack guidance method with high aiming precision is proposed. In BVR air combat, the best launching conditions can be formed through the attack guidance and aiming of fighters, which can give full play to the combat effectiveness of BVR AAMs to the greatest extent. The mode of manned fighters aiming by manual control of pilots is inefficient and obviously not suitable for the autonomous UCAV. Existing attack guidance control methods have some defects such as low precision, poor timeliness, and too much reliance on manual experience when intercepting highly maneuvering targets. To address this problem, aiming error angle is calculated based on the motion model of UCAV and the aiming model of BVR attack fire control in this study, then target motion prediction information is introduced based on the designed model predictive control (MPC) framework, and the adaptive fuzzy guidance controller is designed to generate control variable. To reduce the predicted aiming error angle, the algorithm iteratively optimizes and updates the actual guidance control variable online. The simulation results show that the proposed method is very effective for solving the autonomous attack guidance problem, which has the characteristics of adaptivity, high timeliness, and high aiming precision.
引用
收藏
页数:21
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