Safety-Critical Control of Quadrotor UAVs with Control Barrier Functions

Tianyi Yang, Zhiqiang Miao, Guo Yi, Yaonan Wang
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Abstract

For quadrotors, imposing multiple dynamic constraints on the state simultaneously to achieve safe control is a challenging problem. In this paper, a cascaded control archi-tecture based on quadratic programming method is proposed to generate minimally-invasive and collision-free control actions. This architecture consists of exponential control barrier functions(ECBFs) to construct a non-conservative forward invariant safety region and geometric nonlinear PID attitude control with considering quadrotor dynamics to avoid the singularities of Euler-angles and the ambiguity of quaternions. The feasibility and the effectiveness of the proposed cascaded control architecture is demonstrated through numerical simulations.
具有控制屏障功能的四旋翼无人机安全临界控制
对于四旋翼飞行器来说,同时对其状态施加多个动态约束以实现安全控制是一个具有挑战性的问题。本文提出了一种基于二次规划方法的级联控制体系结构,以产生最小侵入性和无碰撞的控制动作。该体系结构由指数控制屏障函数(ECBFs)和几何非线性PID姿态控制组成,前者用于构造非保守的前向不变安全区域,后者考虑了四旋翼动力学,避免了欧拉角的奇异性和四元数的模糊性。通过数值仿真验证了所提出的级联控制结构的可行性和有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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