面向低空起降场的UWB定位基站拓扑结构通用性设计方法

A generalizable UWB anchor deployment design method for low-altitude takeoff and landing sites

  • 摘要: 针对传统超宽带 (ultra wide band,UWB)定位基站拓扑设计忽视起降场任务域特征,导致峰值误差与连续失效风险难以约束的问题,本文提出一种面向起降过程的UWB基站拓扑结构通用性设计方法. 首先对平台三维空间、起降轨迹及走廊保障域进行建模,构建同时表征几何质量、误差鲁棒性、连续可用性与走廊覆盖率的优化目标模型;随后在离散候选点与工程部署约束下,引入萤火虫算法进行求解,获得面向任务的最优拓扑. 结果表明,该方法在4~6个基站规模下均获得更优且更稳健的综合性能:最大连续失效长度可降至0,走廊覆盖率均达到100%,并在误差95%分位等关键指标上表现突出,能在关键航段有效抑制几何退化与误差尾部. 该方法具有良好的工程可迁移性,可为低空起降场UWB基站部署提供依据.

     

    Abstract: Traditional UWB (ultra-wide band) localization anchor topology design often overlooks the mission-domain characteristics of takeoff and landing sites, which makes peak positioning errors and continuous outages difficult to be controlled. In order to solve this problem, a generalizable UWB anchor topology design method for takeoff and landing operations is proposed. First, the 3D platform space, takeoff/landing trajectories, and the corridor protection region are modeled. An optimization model is formulated to jointly characterize geometric quality, error robustness, continuous availability, and corridor coverage. Then, under discretized candidate locations and engineering deployment constraints, a Firefly Algorithm is employed to obtain the mission-oriented optimal topology. Results show that the proposed method achieves superior and more robust overall performance for M = 4, 5 and 6. the maximum continuous failure length can be reduced to zero, the corridor coverage rate reaches 100%, and key metrics such as the 95th percentile positioning error can be improved, and geometric degradation and error tails on critical flight segments can be suppressed. The proposed method is readily transferable to engineering practice and provides practical guidance for UWB anchor deployment in low-altitude takeoff and landing sites.

     

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