Ke Yuan

Large deployable mesh reflectors (DMRs) play a vital role in spaceborne communication and observation systems because of their low mass and compact stowage capability. Nevertheless, maintaining stringent surface accuracy while mitigating pronounced thermal influences in the orbital environment remains a persistent engineering challenge. This study develops a spatially discretized thermal modeling framework that incorporates direct solar radiation, Earth albedo, a prescribed equivalent Earth‐infrared heat input, section‐dependent solar‐exposure factors, structural self‐shadowing, and reflector emission to space. The proposed method is implemented to modeling of an 817‐node center‐feed reflector and an 849‐node offset‐feed reflector. Each reflector is discretized into one to 10 spatial sections and analyzed over four idealized geostationary‐orbit eclipse‐season cycles. Temperature distributions are evaluated at representative spatial nodes, and the influence of spatial discretization is quantified using normalized absolute temperature differences referenced to the 10‐section model. For the center‐feed reflector, the section‐dependent temperature field is further converted into thermal strains and thermally modified stress‐free cable lengths, and the resulting shape distortion of its reflecting surface is evaluated using the direct root‐mean‐square surface error.

Tensegrity structures become important components of various engineering structures due to their high stiffness, light weight, and deployable capability. Existing studies on their dynamic analyses mainly focus on responses of their nodal points while overlook deformations of their cable and strut members. This study proposes a non-contact approach for the experimental modal analysis of a tensegrity structure to identify its three-dimensional (3D) natural frequencies and full-field mode shapes, which include modes with deformations of its cable and strut members. A 3D scanning laser Doppler vibrometer is used with a mirror for extending its field of view to measure full-field vibration of a novel three-strut metal tensegrity column with free boundaries. Tensions and axial stiffnesses of its cable members are determined using natural frequencies of their transverse and longitudinal modes, respectively, to build its theoretical model for dynamic analysis and model validation purposes. Modal assurance criterion (MAC) values between experimental and theoretical mode shapes are used to identify their paired modes. Modal parameters of the first 15 elastic modes of the tensegrity column identified from the experiment, including those of the overall structure and its cable members, can be classified into five mode groups depending on their types. Modes paired between experimental and theoretical results have MAC values larger than 78%. Differences between natural frequencies of paired modes of the tensegrity column are less than 15%. The proposed non-contact 3D vibration measurement approach allows accurate estimation of 3D full-field modal parameters of the tensegrity column.

Developing a miniatured laser vibrometer becomes important for many engineering areas, such as experimental and operational modal analyses, model validation, and structural health monitoring. Due to its compact size and light weight, a miniatured laser vibrometer can be attached to various mobilized platforms, such as an unmanned aerial vehicle and a robotic arm whose payloads can usually not be large, to achieve a flexible vibration measurement capability. However, integrating optics into a miniaturized laser vibrometer presents several challenges. These include signal interference from ghost reflectance signals generated by the sub-components of integrated photonics, polarization effects caused by waveguide structures, wavelength drifting due to the semiconductor laser, and the poorer noise characteristics of an integrated laser chip compared to a non-integrated circuit. This work proposes a novel chip-based high-precision laser vibrometer by incorporating two or more sets of quadrature demodulation networks into its design. An additional set of quadrature demodulation networks with a distinct reference arm delay line length can be used to conduct real-time compensation to mitigate linear interference caused by temperature and environmental variations. A series of vibration measurements with frequencies ranging from 0.1 Hz to 1 MHz were conducted using the proposed laser vibrometer to show its repeatability and accuracy in vibration and ultrasonic vibration measurements, and its robustness to test surface conditions. The proposed laser vibrometer has the advantage of directly measuring the displacement response of a vibrating structure rather than integrating its velocity response to yield the measured displacement with a conventional laser Doppler vibrometer.