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arXiv 2603.08045eess.SYcs.ROcs.SY

自主直升机轨迹跟踪控制设计:保证误差界限

Trajectory Tracking Control Design for Autonomous Helicopters with Guaranteed Error Bounds

Institute of Flight Systems, German Aerospace Center (DLR)(飞行系统研究所,德国航天中心);Institute for Production Technology and Systems, Leuphana University of Lueneburg(生产技术与系统研究所,路比哈大学)

Philipp Schitz, Johann C. Dauer, Paolo Mercorelli

AI总结:

本文提出基于RPI集的自主直升机轨迹跟踪控制设计,通过计算保证误差界限并比较不同控制器架构的性能与保守性。

摘要:

本文提出了一种系统框架,用于基于鲁棒正不变集(RPI集)计算自主直升机轨迹跟踪误差的正式保证界限。该方法聚焦于建立闭环位移误差动力学,将其转化为多面体线性参数变换形式,并包含有界附加和状态依赖的扰动。计算出椭球RPI集,得到明确的位置误差界限,可作为上层轨迹规划中的认证缓冲区。三种控制器架构在误差界限的保守性和跟踪性能方面进行了比较。非线性直升机模型的仿真结果表明,所有架构都遵守推导出的界限,同时突显了在不变集计算中动态保真度和保守性之间的权衡。

英文摘要:

This paper presents a systematic framework for computing formally guaranteed trajectory tracking error bounds for autonomous helicopters based on Robust Positive Invariant (RPI) sets. The approach establishes a closed-loop translational error dynamics which is cast into polytopic linear parameter-varying form with bounded additive and state-dependent disturbances. Ellipsoidal RPI sets are computed, yielding explicit position error bounds suitable as certified buffer zones in upper-level trajectory planning. Three controller architectures are compared with respect to the conservatism of their error bounds and tracking performance. Simulation results on a nonlinear helicopter model demonstrate that all architectures satisfy the derived bounds, while highlighting trade-offs between performance and the conservatism of the computed invariant set.

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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