arXiv:2607.13703cs.LGcs.SY2026-07

用可逆神经网络实现无人机精准控制,效果接近经典方法。

Conditional Invertible Neural Networks for Data-Driven UAV Control: A 2-D Proof of Concept

论文配图:Conditional Invertible Neural Networks for Data-Driven UAV Control: A 2-D Proof of Concept
图 1 · 摘自论文原文
  • 设计条件可逆网络建模无人机逆动力学,支持概率控制决策。
  • 闭环测试中位置误差仅略高于经典方法(9.7 vs 9.5米),47%场景跟踪达标。
  • 揭示控制失败主因:指令带宽不足与数据覆盖不全,指导系统优化。

本文研究条件可逆神经网络(cINNs)作为多旋翼无人机的统计逆动力学模型。针对平面X8共轴多旋翼,利用增量非线性动态逆(INDI)教师模型,通过有理二次样条耦合与可逆线性混合学习 $p(u ackslashmid s_t, c_t)$。开环复现达到 $R^2 = 0.944$,平均CRPS为0.0915,对数似然误差相关系数 $ρ= -0.60$。在超过15个闭环场景中,位置均方根误差与INDI相当(9.7米 vs 9.5米),47%场景实现可接受跟踪;失败模式分为激进指令下的姿态发散与高频参考下的相位滞后,明确指出指令带宽和数据覆盖是主要失效机制。

原文摘要 · Abstract (English)

We investigate conditional invertible neural networks (cINNs) as probabilistic inverse-dynamics models for multirotor control. For a planar X8 coaxial multicopter, we learn $p(u \mid s_t, c_t)$ from an incremental nonlinear dynamic inversion (INDI) teacher using rational-quadratic spline coupling and invertible linear mixing. Open-loop reproduction reaches $R^2 = 0.944$, mean CRPS 0.0915, and log-probability-error correlation $ρ= -0.60$. Over 15 closed-loop scenarios, position RMSE matches INDI (9.7 vs. 9.5 m), with 47 percent tracking acceptably; failures separate into attitude divergence under aggressive steps and phase lag under high-frequency references, isolating command bandwidth and data coverage as dominant failure mechanisms.

无人机控制可逆网络概率建模

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