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视场约束下三维时变速度攻击时间控制制导律(飞行器协同作战专栏)

周军,黄晓阳,赵斌   

  1. 西北工业大学
  • 收稿日期:2026-04-27 修回日期:2026-07-16 出版日期:2026-07-20 发布日期:2026-07-20
  • 通讯作者: 赵斌
  • 基金资助:
    国家自然科学基金

Three-dimensional impact-time-control guidance law with field-of-view constraint and time-varying velocity

  • Received:2026-04-27 Revised:2026-07-16 Online:2026-07-20 Published:2026-07-20
  • Contact: Bin ZHAO

摘要: 针对多飞行器协同打击固定目标三维场景中,攻击时间约束、导引头视场约束、速度时变与几何耦合导致时间控制精度与飞行轨迹可行性难以兼顾的问题,提出一种三维解析攻击时间控制制导律。该方法以标准攻击平面为动态几何参考,构造轨迹收敛通道以约束速度方向纵向演化;构造三维等效时间控制通道,并结合含气动阻力的速度衰减模型,推导视场约束下可达攻击时间区间;再通过解析控制分配将两通道映射为闭式三维加速度指令。收敛性分析表明,在解析模型及一致非奇异工作域内,所提方法保证速度方向渐近贴合标准攻击平面,视场约束全程满足,实际攻击时刻精确收敛于期望攻击时刻,且控制指令有界。仿真结果表明,在完整气动与指令限幅仿真中,所提方法在满足视场约束的同时仍保持较高的攻击时间控制精度;在初始状态、气动参数与目标位置多源联合拉偏的蒙特卡罗仿真中,所提方法仍保持较高的攻击时间控制精度与命中精度,并全程满足视场与正高度约束,具有较强的鲁棒性。

关键词: 三维制导律, 攻击时间控制, 视场约束, 速度时变, 标准攻击平面, 协同打击

Abstract: To address the difficulty of simultaneously ensuring impact-time control accuracy and flight-trajectory feasibility in three-dimensional multi-vehicle cooperative engagement against a fixed target, where impact-time constraints, seeker field-of-view (FOV) constraints, time-varying velocity, and geometric coupling are involved, this paper proposes a three-dimensional analytical impact-time-control guidance law. The proposed method uses the standard engagement plane as a dynamic geometric reference and constructs a trajectory convergence channel to constrain the longitudinal evolution of the velocity direction. A three-dimensional equivalent time-control channel is then extracted, and a velocity decay model with aerodynamic drag is incorporated to analytically determine the reachable impact-time interval under the FOV constraint. The two channels are further mapped into closed-form three-dimensional acceleration commands through analytical control allocation. The convergence analysis shows that, within the operating domain where the control allocation matrix is uniformly nonsingular, the proposed method guarantees asymptotic alignment of the velocity direction with the standard engagement plane, continuous satisfaction of the FOV constraint, accurate convergence of the actual impact time to the desired impact time, and bounded control commands. Simulation results demonstrate that, under nominal conditions, the proposed method achieves satisfactory impact-time control accuracy while satisfying the FOV constraint. In Monte Carlo simulations with combined deviations of the initial states, aerodynamic parameters, and target position, the proposed method still maintains satisfactory impact-time control accuracy and homing accuracy, while the FOV and positive-altitude constraints are satisfied throughout the engagement, demonstrating considerable robustness.

Key words: three-dimensional guidance, impact-time control, field-of-view constraint, time-varying velocity, standard engagement plane, cooperative strike

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