المؤلفون: Shilei Cao, Man Yang, Jian Liu

المصدر: Aerospace, Vol 11, Iss 1, p 54 (2024)

مصطلحات موضوعية: continuum modeling, boundary control, flexible satellite, large space truss structure, vibration control, Motor vehicles. Aeronautics. Astronautics, TL1-4050

Relation: https://www.mdpi.com/2226-4310/11/1/54; https://doaj.org/toc/2226-4310; https://doaj.org/article/77590b17a9d34958b8a076ae15a99eee

الاتاحة: https://doi.org/10.3390/aerospace11010054
https://doaj.org/article/77590b17a9d34958b8a076ae15a99eee