临近空间高速飞行器防御制导律发展与分析
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1.国防科技大学 先进推进技术实验室;2.西安工业大学 基础学院

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V11

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国家自然科学基金资助项目(12502052);国家资助博士后研究人员计划(GZB20240989);中国博士后科学基金(2024M754304);智能博弈重点实验室创新工作站开放课题(ZBKF-24-01);湖南省自然科学基金资助项目(2025JJ60072)


Development and Analysis of Defense Guidance Laws for High-Speed Vehicles in Near Space
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    摘要:

    当前世界各国普遍缺乏有效防御高速飞行器的能力,相关基础研究仍处于起步阶段,加快发展高速目标防御技术对维护空天安全具有重要意义。针对此背景下临近空间防御对抗中存在的防御态势狭窄、速度劣势明显、单弹防御力弱等问题,对当前临近空间高速飞行器防御制导律的发展现状进行综述,分别从复杂攻防对抗场景、导弹协同制导机理、真实环境效能约束等方面剖析现有制导律研究的不足,并展望了未来高速飞行器防御制导律的重点发展方向,旨在为未来高速飞行器防御体系建设和精确制导领域的前沿基础研究提供参考。

    Abstract:

    Currently, countries around the world are generally unable to defend effectively against high-speed vehicles, and related basic research is still in its infancy. Accelerating the development of high-speed target defense technology is crucial for maintaining aerospace security. Given the problems present in the near-space defense confrontation under this background, such as a narrow defensive posture, significant speed disadvantages, and limited single-missile defense capability, this paper reviews the current development status of the defense guidance law for high-speed near-space vehicles. It analyzes the deficiencies of the existing guidance law research from perspectives such as complex offensive and defensive confrontation scenarios, missile cooperative guidance mechanisms, and real environment effectiveness constraints. It also foresees the key development directions of future defense guidance laws for high-speed vehicles, aiming to offer references for the construction of future defense systems for high-speed vehicles and the frontier basic research in the field of precision guidance.

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  • 收稿日期:2025-10-30
  • 最后修改日期:2025-12-17
  • 录用日期:2026-01-12
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