旋翼式星表探测六杆张拉整体机器人非线性力学建模及碰撞仿真分析

Nonlinear Mechanical Modeling and Collision Simulation Analysis on Rotor Six-bar Tensegrity Robot for Star Catalog Detection

  • 摘要: 针对星表环境中旋翼式机器人因碰撞导致螺旋桨损坏的问题,提出一种基于六杆张拉整体结构的防碰撞旋翼式机器人构形。通过构建节点矩阵、连接矩阵及向量矩阵,建立六杆张拉整体结构的数学模型,并采用基于平衡矩阵与非线性有限元理论的求解方法进行力学分析。借助 HyperMesh 软件对简化的 3 维模型进行网格划分,将 3 维网格模型导入 ABAQUS 软件开展不同跌落与飞行速度下的碰撞仿真,以结构干涉及变形程度为评价准则验证其防碰撞性能。仿真结果表明,该机器人在发生跌落时,以闭合三角面接触土卫六表面,可以承受高达23.7 m 的最大跌落高度,其螺旋桨设计能够确保在此过程中免受损坏。在旋翼杆遭遇碰撞的情况下,该结构能够承受 7 m/s 的冲击速度。最终,通过搭建样机并进行静态与动态载荷测试,进一步验证了所提构形的有效性。综上,本研究中的旋翼式机器人防碰撞能力覆盖了正常着陆操作中可能遇到的意外情况,为星表探测任务中的机器人安全性与可靠性提供了创新性的技术解决方案。

     

    Abstract: Aiming at the problem of propeller damage caused by collision of rotor-type robots in star catalog environment,an anti-collision rotor-type robot configuration based on six-bar tensegrity structure is proposed. By constructing the node matrix, connection matrix and vector matrix, the mathematical model of the six-bar tensegrity structure is established, and the mechanical analysis is carried out by using the solution method based on the equilibrium matrix and nonlinear finite element theory. The simplified 3D model is meshed by HyperMesh software, and the 3D mesh model is imported into ABAQUS software to carry out collision simulation under different drop and flight speeds. The anti-collision performance is verified by the evaluation criteria of structural interference and deformation degree. The simulation results show that when the robot falls, it contacts the surface of Titan with a closed triangular surface, and can withstand a maximum drop height of up to23.7 m. Design of its propeller ensures protection from damage during this process. In the case of a collision against the rotor bar, the structure can withstand the impact velocity of 7 m/s. Finally, the effectiveness of the proposed configuration is further verified by building a prototype and performing static and dynamic load tests. In summary, the anti-collision capability of the rotor-type robot in this study covers unexpected situations that may be encountered during normal landing operations,providing an innovative technical solution for robot safety and reliability in star catalog detection.

     

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