This paper presents a theoretical study on the ability of multi-rotor aerial vehicles (MRAVs) with tiltable propellers to achieve and sustain static hovering at different orientations. To analyze the ability of MRAVs with tiltable propellers to achieve static hovering, a novel linear map between the platform's control inputs and applied forces and moments is introduced. The relation between the introduced map and the platform's ability to hover at different orientations is developed. Correspondingly, the conditions for MRAVs with tiltable propellers to realize and sustain static hovering are detailed. A numerical metric is then introduced, which reflects the ability of MRAVs to sustain static hovering at different orientations. A subclass of MRAVs with tiltable propellers is defined as the Critically Statically Hoverable platforms (CSH), where CSH platforms are MRAVs that cannot sustain static hovering with fixed propellers, but can achieve static hovering with tilting propellers. Finally, extensive simulations are conducted to test and validate the above findings, and to demonstrate the effect of the proposed numerical metric on the platform's dynamics.
翻译:本文介绍了关于具有可倾斜螺旋桨的多旋转航空飞行器(MRAVs)在不同方向实现和保持静态悬浮的能力的理论研究。为了分析带有可倾斜螺旋桨的MRAVs实现静悬浮的能力,介绍了平台控制投入与应用力和瞬时之间的新的线性图。正在开发所介绍的地图与平台在不同方向上悬浮的能力之间的关系。相应的,详细介绍了带有可倾斜螺旋桨的MRAVs实现和保持静态悬浮的能力。随后采用了一个数字指标,反映了可倾斜螺旋桨的MRAVs保持在不同方向静悬浮的能力。一个带有可倾斜螺旋桨的亚类MRAVs子类被定义为临界的可变光平台,其中CSH平台无法用固定螺旋桨维持静态悬浮,但能够用倾斜螺旋桨实现静态悬浮。最后,进行了广泛的模拟,以测试和验证上述结果,并展示拟议的数字矩阵对平台动态的影响。