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arXiv 2606.28827cs.RO

LNN-Fly:时序失配下鲁棒避障的连续时间无人机导航

LNN-Fly: Continuous-Time UAV Navigation for Robust Obstacle Avoidance under Timing Mismatch

Shenzhen Institute for Advanced Study, University of Electronic Science and Technology of China(深圳先进研究院,电子科技大学)

Yulin Huang, Shaojie Chen, Di Feng, Jiahao Wang, Ping Liu, Jianxiao Zou

AI总结:

提出LNN-Fly,一种面向部署的连续时间导航策略,通过动态规划启发的结构化循环更新、显式控制间隔条件和自适应遗忘门,在时序失配下实现鲁棒避障,并在仿真和实物中验证了有效性。

摘要:

端到端无人机导航在仿真中可实现令人印象深刻的敏捷性,但其避障行为在部署后往往会退化,因为策略必须容忍仿真器失配、感知不规则和变速率控制。这些效应在杂乱环境中尤其危险,过时的观测或短暂的控制不规则可能直接导致碰撞。我们提出LNN-Fly,一种面向部署的连续时间导航策略,用于基于LiDAR的无人机避障。该策略结合了动态规划启发的结构化循环更新、对已过控制间隔Δt的显式条件化,以及一个输入驱动的自适应遗忘门,该门在危险附近刷新过时的潜在状态,同时在持续机动中保持一致性。它通过包含部署相关感知和时间扰动的可微轨迹进行训练。在仿真中,LNN-Fly在测试设置中提高了避障性能,并显示出对降低控制频率、稀疏观测和控制周期抖动的更好容忍度。它还能从简化的可微仿真器零样本迁移到物理四旋翼。在室内跨频率真实世界测试中,系统在20次飞行中实现了100%的成功率,而策略推理在桌面GPU上的中位延迟为0.514毫秒,在机载CPU上约为2.5毫秒,机载P95延迟低于30毫秒。

英文摘要:

End-to-end unmanned aerial vehicle (UAV) navigation can achieve impressive agility in simulation, yet its obstacle-avoidance behavior often degrades after deployment because the policy must tolerate simulator mismatch, sensing irregularity, and variable-rate control. These effects are especially dangerous in cluttered environments, where stale observations or short control irregularities can directly lead to collisions. We present LNN-Fly, a deployment-oriented continuous-time navigation policy for LiDAR-based UAV obstacle avoidance. The policy combines a dynamic-programming-inspired structured recurrent update, explicit conditioning on the elapsed control interval Δt, and an input-driven adaptive forgetting gate that refreshes stale latent state near hazards while preserving consistency during sustained maneuvers. It is trained with differentiable rollouts that incorporate deployment-relevant sensing and timing perturbations. In simulation, LNN-Fly improves obstacle-avoidance performance in the tested settings and shows better tolerance to reduced control frequency, sparse observations, and control-period jitter. It also transfers zero-shot from a simplified differentiable simulator to a physical quadrotor. In indoor cross-frequency real-world tests, the system achieves 100% success over 20 flights, while policy inference has a median latency of 0.514 ms on a desktop graphics processing unit (GPU) and about 2.5 ms on the onboard central processing unit (CPU), with onboard P95 latency below 30 ms.

机构、总结、中文摘要均由AI分析而来,可能存在错误,请以论文正文为准。

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