多无人机协同突防拦截静止目标,仅部分带雷达,其余靠通信协作。
Predefined-time One-Shot Cooperative Estimation, Guidance, and Control for Simultaneous Target Interception
- 部分无人机带雷达,其余通过通信获取目标信息并协作拦截
- 设计预设时间收敛的观测器与制导指令,确保同步命中
- 适用于复杂战场环境下的协同拦截任务,适合多机系统研究者
本文提出一种统一的非线性估计-制导-控制框架,用于在异构感知拓扑下协同同时拦截静止目标。仅有部分无人机配备机载导引头(有源/导引头型),其余无人机(无导引头型)通过有源邻居间接获取目标信息,并执行分布式协同制导以实现同时拦截。针对由此产生的部分可观测性问题,采用预设时间分布式观测器,通过有向通信图实现无导引头型无人机对目标状态估计的收敛。随后,利用考虑大发射包络的改进时间至相遇估计,设计分布式协同制导指令,该估计与预设时间一致性协议耦合,确保各无人机时间至相遇值达成一致。观测误差和时间至相遇一致性误差可在预设时间内收敛至零。制导指令通过自动驾驶仪实现,使用鸭舵控制,采用预设时间收敛的滑模控制律生成舵面偏转指令,使自动驾驶仪在指定时间内精确跟踪侧向加速度指令,且整体设计非奇异。理论分析经多种交战几何下的数值仿真验证,证明了估计精度、协同拦截性能及自动驾驶响应能力。
原文摘要 · Abstract (English)
This work develops a unified nonlinear estimation-guidance-control framework for cooperative simultaneous interception of a stationary target under a heterogeneous sensing topology, where sensing capabilities are non-uniform across interceptors. Specifically, only a subset of agents is instrumented with onboard seekers (informed/seeker-equipped agents), whereas the rest of them (seeker-less agents) acquire the information about the target indirectly via the informed agents and execute a distributed cooperative guidance for simultaneous target interception. To address the resulting partial observability, a predefined-time distributed observer is leveraged, guaranteeing convergence of the target state estimates for seeker-less agents through information exchange with seeker-equipped neighbors over a directed communication graph. Thereafter, an improved time-to-go estimate accounting for wide launch envelopes is utilized to design the distributed cooperative guidance commands. This estimate is coupled with a predefined-time consensus protocol, ensuring consensus in the agents' time-to-go values. The temporal upper bounds within which both observer error and time-to-go consensus error converge to zero can be prescribed as design parameters. Furthermore, the cooperative guidance commands are realized by means of an autopilot, wherein the interceptor is steered by canard actuation. The corresponding fin deflection commands are generated using a predefined-time convergent sliding mode control law. This enables the autopilot to precisely track the commanded lateral acceleration within a design-specified time, while maintaining non-singularity of the overall design. Theoretical guarantees are supported by numerical simulations across diverse engagement geometries, verifying the estimation accuracy, the cooperative interception performance, and the autopilot response using the proposed scheme.
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