Control of a service satellite during its mission on space debris removal from orbits with high inclination by implementation of an ion beam method

Obukhov, V. A.; Kirillov, V.A.; Petukhov, V. G.; Pokryshkin, A.I.; Popov, G.A.; Svotina, V. V.; Testoyedov, N. A.; Usovik, I.V.

doi:10.1016/j.actaastro.2021.09.041

Cited by 8 publications

(2 citation statements)

References 13 publications

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“…If there is a chance of a close intersection for two space debris with different orbital inclinations, the time window of the leap is near to the ascending or descending intersection point. According to Formula (3), it is necessary to meet the following conditions in Equation ( 6) [27]:…”

Section: Centimeter Space Debris Removal Scenementioning

confidence: 99%

Target Selection for a Space-Energy Driven Laser-Ablation Debris Removal System Based on Ant Colony Optimization

Yang

Shao

et al. 2023

Sustainability

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The space-energy driven laser-ablation debris removal technology can remove or detach multiple centimeter-level space debris in a single mission. However, the space-energy driven platform can only rely on its own equipment capabilities to detect and identify space debris. It is necessary to select multiple potentially removable debris targets to improve the removal efficiency. In this paper, target selection for a space-energy driven laser-ablation debris removal system is analyzed based on ant colony optimization. The intersection and interaction periods were given by the optimal driving sequence calculation for multiple debris. Parameters such as the detection range, pulsed energy, repetition frequency of the laser and trajectory of debris have been considered as inputs of the simulation. Target selection and optimal action time have been calculated when a single debris entered the detection range of the laser system. This optimization can significantly improve the overall efficiency and laser energy utilization of the space-based laser platform for the same randomly generated debris group, compared to the mode driven sequentially according to the order of entering the laser action range. The results showed that after being filtered by the ant colony algorithm, the number of removable debris doubled, and the de-orbit altitude increased by 15.9%. The energy utilization rate of the laser removal system has been improved by 74.6%. This optimization algorithm can significantly improve the overall work efficiency and laser energy utilization rate of the space-energy driven system. It can remove more debris or have a larger effective orbit reduction distance value for all debris.

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Section: Centimeter Space Debris Removal Scenementioning

confidence: 99%

Target Selection for a Space-Energy Driven Laser-Ablation Debris Removal System Based on Ant Colony Optimization

Yang

Shao

et al. 2023

Sustainability

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“…Spacecraft is widely applied in some space missions (Flores-Abad et al, 2014; Obukhov et al, 2022; Waswa et al, 2013; Wilde et al, 2014; Xu, 2021). It is not only a highly coupled nonlinear system but also suffers from uncertainties and time-varying external disturbances (Zheng and Song, 2014; Xie et al, 2021).…”

Section: Introductionmentioning

confidence: 99%

Immersion and invariance sliding mode control with time-delay estimation for rigid spacecraft with uncertainties and actuator faults

Jing

Liu

et al. 2023

Transactions of the Institute of Measurement and Control

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This paper investigates the attitude control of rigid spacecraft with uncertainties and actuator faults. An immersion and invariance sliding mode control with time-delay estimation (IISMCTDE) is proposed to cope with uncertainties, disturbances, and actuator faults. First, time-delay estimation is utilized to reconstruct the total disturbances including uncertainties, disturbances, and actuator faults. Then, based on the time-delay estimation, an immersion and invariance sliding mode control (IISMC) scheme is developed to achieve accurate attitude tracking from the reconstructed knowledge. The proposed IISMCTDE can not only achieve finite-time convergence but also be simple and easy to operate. Simulations are provided to demonstrate the effectiveness of the proposed approach.

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Dynamics of relative translation motion of spherical space debris during ion beam transportation

Aslanov¹,

Ledkov²

2023

Attitude Dynamics and Control of Space Debris During Ion Beam Transportation

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Control of a service satellite during its mission on space debris removal from orbits with high inclination by implementation of an ion beam method

Cited by 8 publications

References 13 publications

Target Selection for a Space-Energy Driven Laser-Ablation Debris Removal System Based on Ant Colony Optimization

Target Selection for a Space-Energy Driven Laser-Ablation Debris Removal System Based on Ant Colony Optimization

Immersion and invariance sliding mode control with time-delay estimation for rigid spacecraft with uncertainties and actuator faults

Dynamics of relative translation motion of spherical space debris during ion beam transportation

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