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A Three-Dimensional Cooperative Guidance Law Based on Consensus Theory for Maneuvering Targets

机译:基于协商目标的三维合作指导法律

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摘要

In this paper, a cooperative guidance law based on consensus theory is proposed for multiple flight vehicles against a maneuvering target in a three-dimensional plane. The proposed guidance law has three orientation components: the one along the line-of-sight (LOS) ensures that all flight vehicles reach the target simultaneously, and the other two normal to the LOS in longitudinal and lateral plane guarantee the accurate interception. The target maneuverings are estimated by a finite-time convergence disturbance observer (FTDOB) and are compensated into the kinematic equation to achieve more accurate interception. Using the Lyapunov stability theorem, time-to-go of all flight vehicles' convergence is proved. Mathematical simulations verify the effectiveness of the proposed cooperative guidance law.
机译:本文提出了一种基于共识理论的合作指导法,用于在三维平面上对机动目标的多个飞行车辆。拟议的指导法有三个定向组件:沿着视线(LOS)的一个方向组成部分确保所有飞行车辆同时到达目标,并且在纵向和横向平面上的LOS中的另一个正常情况保证了准确的拦截。通过有限时间的收敛干扰观察者(FTDOB)估计目标机动,并被补偿到运动方程中以实现更准确的拦截。使用Lyapunov稳定性定理,证明了所有飞行器的收敛时间。数学模拟验证了拟议的合作指导法的有效性。

著录项

  • 来源
    《Mathematical Problems in Engineering》 |2019年第15期|37.1-37.11|共11页
  • 作者

    Zhang Wenjie; Du Xiao; Xia Qunli;

  • 作者单位

    Beijing Inst Technol Sch Aerosp Engn Beijing 100081 Peoples R China;

    China Acad Launch Vehicle Technol Beijing 100076 Peoples R China;

    Beijing Inst Technol Sch Aerosp Engn Beijing 100081 Peoples R China;

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  • 正文语种 eng
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