Simplex Sliding Mode Control Strategies for Spacecraft Rendezvous Maneuvers

被引：2

作者：

Capello, Elisa ^{[1
]}

Punta, Elisabetta ^{[2
]}

Bartolini, Giorgio ^{[3
]}

机构：

[1] Politecn Torino, Dept Mech & Aerosp Engn, CNR IEHT, Corso Duca Abruzzi 24, I-10129 Turin, Italy

[2] Politecn Torino, CNR IEHT, Corso Duca Abruzzi 24, I-10129 Turin, Italy

[3] CNR IEHT, Via Marini 6, I-16149 Genoa, Italy

来源：

IFAC PAPERSONLINE | 2017年 / 50卷 / 01期

关键词：

Satellite control applications; Sliding mode control; Control algorithms; Aerospace control; Autonomous control; SYSTEMS;

D O I：

10.1016/j.ifacol.2017.08.824

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Space systems are subject to strict requirements in terms of relative position between two spacecraft and are controlled by actuators, which can perform limited output levels at low frequency. The aim of this work is the design of a sliding mode controller, which suitably combines simplex and super-twisting algorithms. This controller permits to reduce the number of thrusters required to control the spacecraft, the fuel consumption and the switching frequency at which the mono-directional actuators are turned on. The proposed control strategy can be easily converted in an on-board algorithm, with a minimum computational effort. Extensive simulations are carried out to validate the performance of the proposed sliding mode design. (C) 2017, IFAC (International Federation of Automatic Control) Hosting by Elsevier Ltd. All rights reserved.

引用

页码：8496 / 8501

页数：6

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