Yu Liyuan, Qiao Zhilei, Xing Shichao, Wu Yipeng, Ji Hongli
State Key Laboratory of Mechanics and Control for Aerospace Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China.
Anhui Joint Key Laboratory of Critical Technologies for High-End Copper-Based New Materials, Tongling University, Tongling 244061, China.
Sensors (Basel). 2025 Jun 25;25(13):3958. doi: 10.3390/s25133958.
Active or semi-active vibration control systems require real-time vibration information from controlled structures as feedback. However, integrating vibration sensors into some controlled structures remains a challenge due to factors such as mass and signal lines. This issue is particularly prominent in attachment structures located far from the spacecraft, such as robotic arms and solar panels. This paper presents a miniaturized autonomous inertial sensor that can be easily attached to the controlled structure to acquire vibration data and wirelessly transmit the data. We also establish the relationship between cantilevered structural vibration and the inertial acceleration or angular velocity directly measured by the sensor. Consequently, the feedback information for the control system can be calculated by the processor in real-time. This autonomous inertial sensor consists of an inertial measurement unit (IMU) named BMI088 and a common wireless communication unit. An improved Extended Kalman Filter (EKF) algorithm is employed to enhance the quality of the sensing data in practical environments. The experimental results validated the theoretical model, indicating that the miniaturized inertial sensor effectively captures the bending vibration characteristics of the controlled structure.
主动或半主动振动控制系统需要来自受控结构的实时振动信息作为反馈。然而,由于质量和信号线等因素,将振动传感器集成到一些受控结构中仍然是一个挑战。这个问题在远离航天器的附着结构中尤为突出,比如机器人手臂和太阳能板。本文提出了一种小型化自主惯性传感器,它可以轻松附着在受控结构上以获取振动数据并无线传输数据。我们还建立了悬臂结构振动与传感器直接测量的惯性加速度或角速度之间的关系。因此,控制系统的反馈信息可由处理器实时计算得出。这种自主惯性传感器由一个名为BMI088的惯性测量单元(IMU)和一个普通无线通信单元组成。采用改进的扩展卡尔曼滤波器(EKF)算法来提高实际环境中传感数据的质量。实验结果验证了理论模型,表明该小型化惯性传感器有效地捕捉了受控结构的弯曲振动特性。