Thông tin tài liệu
Nhan đề : | Application of homotopy perturbation method to the radial thrust problem |
Tác giả : | Lorenzo, Niccolai Alessandro A., Quarta Giovanni, Mengali |
Năm xuất bản : | 2022 |
Nhà xuất bản : | Springer |
Tóm tắt : | The dynamics of a spacecraft propelled by a continuous radial thrust resembles that of a nonlinear oscillator. This is analyzed in this work with a novel method that combines the definition of a suitable homotopy with a classical perturbation approach, in which the low thrust is assumed to be a perturbation of the nominal Keplerian motion. The homotopy perturbation method provides the analytical (approximate) solution of the dynamical equations in polar form to estimate the corresponding spacecraft propelled trajectory with a short computational time. The accuracy of the analytical results was tested in an orbital-targeting mission scenario. |
Mô tả: | CC BY |
URI: | https://link.springer.com/article/10.1007/s42064-022-0150-4 https://dlib.phenikaa-uni.edu.vn/handle/PNK/7951 |
Bộ sưu tập | OER - Kỹ thuật điện; Điện tử - Viễn thông |
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