计算机科学
灵活性(工程)
航向(导航)
控制理论(社会学)
非线性系统
网络拓扑
事件(粒子物理)
加速度
运动学
趋同(经济学)
控制(管理)
资源(消歧)
弹道
工程类
人工智能
数学
物理
量子力学
计算机网络
统计
经典力学
天文
经济增长
经济
航空航天工程
操作系统
作者
Abhinav Sinha,Shashi Ranjan Kumar,Dwaipayan Mukherjee
出处
期刊:Journal of Guidance Control and Dynamics
[American Institute of Aeronautics and Astronautics]
日期:2021-02-01
卷期号:44 (2): 328-342
被引量:37
摘要
This work proposes two different three-dimensional (3D) cooperative guidance strategies for a group of interceptors aiming a simultaneous interception of a stationary target. The guidance commands for many-to-one engagement scenario are derived considering nonlinear engagement kinematics and an improved time-to-go estimate that takes the interceptors’ heading errors into account. A resource allocation technique is used, which provides flexibility in apportioning the required lateral acceleration in the pitch and the yaw planes. The proposed strategies use the notions of sliding mode control, which is known for its finite-time convergence and better disturbance rejection capabilities. With the proposed techniques, and under various interaction topologies, the multi-interceptor group is able to simultaneously intercept the target, both at an impact time specified in advance as well as when the impact time is decided during engagement itself. The control is executed in an event-triggered fashion, thereby reducing the resource utilization burden while guaranteeing satisfactory closed-loop performance of the guidance strategies. Finally, various engagement scenarios have been considered in simulations to support the theoretical claims.
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