STOCHASTIC MODEL PREDICTIVE CONTROL FOR SPACECRAFT RENDEZVOUS AND DOCKING VIA A DISTRIBUTIONALLY ROBUST OPTIMIZATION APPROACH
A stochastic model predictive control (SMPC) algorithm is developed to solve the problem of three-dimensional spacecraft rendezvous and docking with unbounded disturbance. In particular, we only assume that the mean and variance information of the disturbance is available. In other words, the probab...
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Published in | The ANZIAM journal Vol. 63; no. 1; pp. 39 - 57 |
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Main Authors | , |
Format | Journal Article |
Language | English |
Published |
Cambridge, UK
Cambridge University Press
01.01.2021
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Abstract | A stochastic model predictive control (SMPC) algorithm is developed to solve the problem of three-dimensional spacecraft rendezvous and docking with unbounded disturbance. In particular, we only assume that the mean and variance information of the disturbance is available. In other words, the probability density function of the disturbance distribution is not fully known. Obstacle avoidance is considered during the rendezvous phase. Line-of-sight cone, attitude control bandwidth, and thrust direction constraints are considered during the docking phase. A distributionally robust optimization based algorithm is then proposed by reformulating the SMPC problem into a convex optimization problem. Numerical examples show that the proposed method improves the existing model predictive control based strategy and the robust model predictive control based strategy in the presence of disturbance. |
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AbstractList | A stochastic model predictive control (SMPC) algorithm is developed to solve the problem of three-dimensional spacecraft rendezvous and docking with unbounded disturbance. In particular, we only assume that the mean and variance information of the disturbance is available. In other words, the probability density function of the disturbance distribution is not fully known. Obstacle avoidance is considered during the rendezvous phase. Line-of-sight cone, attitude control bandwidth, and thrust direction constraints are considered during the docking phase. A distributionally robust optimization based algorithm is then proposed by reformulating the SMPC problem into a convex optimization problem. Numerical examples show that the proposed method improves the existing model predictive control based strategy and the robust model predictive control based strategy in the presence of disturbance. |
Author | ZHANG, KAI LI, ZUOXUN |
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Cites_doi | 10.1016/j.actaastro.2018.03.025 10.1002/rnc.2827 10.1016/j.asr.2018.03.037 10.1017/CBO9780511543388 10.1109/TRO.2010.2044948 10.1109/ACCESS.2017.2767179 10.1016/j.automatica.2008.06.017 10.1016/j.conengprac.2011.09.006 10.1109/TCST.2014.2379639 10.2514/1.30734 10.1016/j.jprocont.2016.03.005 10.1109/ACC.2001.946298 10.1016/j.conengprac.2012.03.009 10.1007/978-1-4471-3398-8 10.2514/2.4211 10.2514/1.62219 10.1049/iet-cta:20050411 10.1007/s10957-006-9084-x 10.1109/TAES.2016.140406 10.1109/TAC.2012.2203054 10.1007/s10957-007-9166-4 |
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SubjectTerms | Aerospace engineering Algorithms Attitude control Computational geometry Convexity Electrical engineering Obstacle avoidance Optimization Predictive control Probability density functions Robust control Space rendezvous Space stations Spacecraft Spacecraft docking Stochastic models |
Title | STOCHASTIC MODEL PREDICTIVE CONTROL FOR SPACECRAFT RENDEZVOUS AND DOCKING VIA A DISTRIBUTIONALLY ROBUST OPTIMIZATION APPROACH |
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