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MODIFIED STEWART PLATFORM FOR SPACECRAFT THRUSTER VECTOR CONTROL

机译:用于航天器推进器矢量控制的改进的斯图尔特平台

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Adaptive or intelligent structures which have the capability for sensing and responding to their environment promise a novel approach to satisfying the stringent performance requirements of future space missions. This paper introduces an intelligent modified Stewart platform as an adaptive thruster mount structure with precision positioning and active vibration suppression capabilities for use in space satellites as an intelligent thruster vector control platform. The intelligent thruster mount would utilize piezoelectric sensors and actuators for precision positioning and active vibration suppression to provide fine-tuning of position tolerance for thruster alignment and low transmissibility of vibration to the satellite structure. Similar intelligent platform, introduced here, may be used for sensitive equipment aboard of the spacecraft to suppress the vibration that resonates throughout the spacecraft structure during a thruster firing, solar panel boom opening/reorientation, etc. This vibration renders sensitive optical or measurement equipment non-operational until the disturbance has dissipated. This intelligent system approach would greatly enhance mission performance by fine tuning attitude control, potentially eliminating the non-operational period as well as minimizing fuel consumption utilized for position correction. The configuration of the intelligent thruster mount system is that of a modified Stewart platform. This system is an intelligent tripod with two in-plane rotational degrees of freedom (2-DOF) for the top device-plate. Precision positioning of this structure is achieved using active members that extend or contract to tilt the upper device-plate where the thruster is mounted. An inverse analysis of a modified Stewart platform is employed to determine the required axial displacement of the active struts for the desired angular tilt of the upper device-plate. The active struts can participate in precision positioning as well as vibration suppression of the upper device-plate where the thruster, i.e., the source of the unwanted vibrations and misalignment, is mounted. The proposed Thruster Vector Control (TVC) intelligent platform offers a promising method for achieving fine tuning of positioning tolerances of a thruster as well as minimizing the effects of the disturbances generated during thruster firing in spacecraft such as a satellite.
机译:具有传感和响应其环境的能力的自适应或智能结构承诺满足未来空间任务的严格性能要求的新方法。本文介绍了一个智能改进的Stewart平台,作为自适应推进器安装结构,具有精密定位和主动振动抑制功能,用于太空卫星作为智能推进器矢量控制平台。智能推进器安装件将利用压电传感器和致动器,用于精密定位和主动振动抑制,以提供适用于推进器对准的位置公差和对卫星结构的振动的低传递性的微调。此处介绍的类似智能平台可用于航天器的敏感设备,以抑制推进器烧制,太阳能电池板臂开口/重新定向等在整个航天器结构中共振的振动。该振动呈现敏感光学或测量设备非 - 在干扰耗散之前,他们这种智能系统方法将通过微调姿态控制极大地提高使使徒性能,可能消除非运营期,以及最小化用于定位校正的燃料消耗。智能推进器安装系统的配置是改进的Stewart平台。该系统是智能三脚架,顶部器件板具有两个面内旋转自由度(2-DOF)。使用延伸或收缩的有源构件实现这种结构的精确定位,以倾斜推进器的上部装置板。采用改进的斯图尔特平台的逆分析来确定用于上部装置板的所需角倾斜的有源支柱所需的轴向位移。主动支柱可以参与精密定位以及安装推进器的上部装置板的振动抑制,即推进器,即不需要的振动和未对准的来源。该提议的推进器矢量控制(TVC)智能平台提供了一种有希望的方法,用于实现推进器的定位公差的微调以及最小化在卫星的航天器中推进器射击过程中产生的扰动的影响。

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