Finite-time soft landing on asteroids using nonsingular terminal sliding mode control

Finite-time soft landing on asteroids using nonsingular terminal sliding mode control
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使用非奇异终端滑模控制在小行星上进行有限时间软着陆

DOI:
10.1177/0142331213495040
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发表时间:
2014-04
影响因子:
1.8
通讯作者:
Guo L
Guo L
中科院分区:
计算机科学4区
文献类型:
--
作者:
Lan Q;Li S;Yang J;Guo L

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Successful future asteroid landing missions require that the control method provides advanced disturbance rejection performance and strong robustness against parameter uncertainties to give higher accuracy and reliability in the complex space environment. Motivated by the requirement for safe and precise soft landing on asteroids, the finite-time soft-landing problem of an asteroid probe is addressed in this paper via a nonsingular terminal sliding mode (NTSM) control technique. The problem is formulated as a two-point boundary-value constraints control problem, where the initial and terminal requirements of the soft-landing problem are all included in the problem formulations. Then, according to the specific characteristics of the problem, an NTSM control law for soft landing on an asteroid is proposed. Simulation results demonstrate that, compared to the widely used traditional sling mode control method, the proposed method provides a much faster convergence rate, higher accuracies, better disturbance rejection properties and stronger robustness against parameter uncertainties.
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