Control of an Assembly of Aerial Vehicles Under Uncertainty

Mohamad T. Shahab, Kévin Garanger, E. Feron
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Abstract

In this paper, we consider the problem of controlling a rigid assembly of aerial vehicles under uncertainty. We consider the case when the positions of the vehicle modules in the assembly structure are unknown, but belong to a finite set. In addition, we consider that each module has only its own measurements available for feedback but not that of the whole assembly, so a decentralized control law is developed. We apply an adaptive switching control approach to control this uncertain system. Given a stabilizing controller for the case when there is no uncertainty, we show that the proposed adaptive approach achieves the control objective under uncertainty by presenting illustrative simulation examples; we provide a case study of a recently proposed novel modular flying system, namely a fractal tetrahedron assembly.
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不确定条件下飞行器组合的控制
本文研究不确定条件下飞行器刚性装配的控制问题。考虑车辆模块在装配结构中的位置未知,但属于有限集合的情况。此外,我们考虑到每个模块只有自己的测量值可用于反馈,而不是整个装配的测量值,因此我们建立了分散控制律。采用自适应开关控制方法对该不确定系统进行控制。给出无不确定性情况下的稳定控制器,通过仿真实例说明所提出的自适应方法在不确定性情况下达到了控制目标;我们提供了一个最近提出的新型模块化飞行系统的案例研究,即分形四面体装配。
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