Orbit selection of the space industrial platform with distributed electrical-power system modules
Heading:
| 1Alpatov, AP, 2Wang, Changqing, 3Lu, Hongshi, 4Lapkhanov, Erik 1Institute of Technical Mechanics of the National Academy of Science of Ukraine and the State Space Agency of Ukraine, Dnipro, Ukraine; 2- School of Automation, Northwestern Polytechnical University, Xi'an, China; 2School of Automation, Northwestern Polytechnical University, Xi'an, China 3School of Automation, Northwestern Polytechnical University, Xi'an, China; 3- Chongqing Innovation Center, Northwestern Polytechnical University, Chongqing, China 4Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine, Dnipro, Ukraine |
| Space Sci. & Technol. 2024, 30 ;(4):03-23 |
| https://doi.org/10.15407/knit2024.04.003 |
| Publication Language: English |
Abstract: Space industrialization is one of the prospective directions in modern aerospace science and engineering for space exploration of new resources and habitats. The key issue is to provide industrial space modules with the required amount of electricity needed. One type of power supply for such modules is the use of distributed power systems, which consist of constellations of spacecraft with contactless power transmission. Given this, the problem of rational orbit selection for their dislocation arises. Considering these problems, the methodology for orbits selection of the space industrial platform with distributed electrical-power system modules is proposed in the paper. This methodology includes orbital translation, attitude, relative dynamics estimation for each power satellite, and its corresponding orbit optimization algorithm.
The orbit optimization algorithm includes statistical processing and elements of gradient and coordinate descent methods, allowing us to determine the most significant parameter influencing the duration of the contactless power transmission session. Also, quaternion mathematics is used to estimate the dynamics in the program parameters for targeting the transmitter spacecraft antenna to the receiver spacecraft rectenna. With the approaches mentioned above, the methodology proposed in this paper allows us to form the requirements for the power satellites’ attitude and orbit control system to improve the process of selecting corresponding design parameters of such systems.
Thus, the usage of the proposed methodology can allow the designing of the power satellites' attitude and orbit control system in the conceptual stages of designing.
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| Keywords: contactless power transmitting; orbit selection; targeting quaternion; optimization of orbit parameters |
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