Abstract
In order to solve the problem of space station’s limited space-ground transportation capacity, this paper studies the space station transit transportation task based on the space tether system. First, the return mission of the test capsule is designed; Then a bead model of the system in near-circular orbit is established; In order to release the test chamber to the specified position under certain conditions, a non-singular fast finite-time closed-loop tracking controller is designed. At the same time, the actual release error is considered, and it is compared with the nominal expansion control law of the tether system under a near circular orbit.; Finally, the simulation results and analysis show that the designed finite-time controller can well deploy the tether release test capsule to the designated position and re-enter the atmosphere. The use of the space tether system to realize the space station load transfer transportation task can provide a good application platform for the space station technology.
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Peijie, S., Changqing, W., Zabolotnov, Y.M., Aijun, L., Qiang, F. (2022). Design of Space Transit Transportation Task Based on Nonsingular Finite-Time Control. In: Yan, L., Duan, H., Yu, X. (eds) Advances in Guidance, Navigation and Control . Lecture Notes in Electrical Engineering, vol 644. Springer, Singapore. https://doi.org/10.1007/978-981-15-8155-7_227
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DOI: https://doi.org/10.1007/978-981-15-8155-7_227
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