Intelligent Fuzzy Control in Stabilizing Solar Sail with Individually Controllable Elements

Author:

Chen Lin1,Fu Xiaoyu2,Ramil Santos1,Xu Ming1ORCID

Affiliation:

1. Beihang University, 100191 Beijing, China

2. Surrey Space Centre, The University of Surrey, GU2 7XH Guildford, UK

Abstract

Fuzzy logical control is a robust and effective control method in industrial fields, which renders it applicable to the attitude control of a solar sail. However, it is hard to apply in black-box and time-varying problem as real solar sail attitude control. Considering the lack of a priori knowledge and the unacceptable manual workload in the design of the fuzzy logical controller (FLC), an intelligent FLC designer (IFLCD) is developed by introducing neural network modelling and automatic design method. Besides, IFLCD also supports self-adaption for better control accuracy. By applying the proposed IFLCD in the attitude stabilization of a solar sail with individually controllable elements (SSICE), an effective solution of unmanned, time-varying, and complex system control method is offered without any mathematical model, which also overcomes the difficulties in FLC design Considering the performance degradation, accident, and distance problems faced by spacecraft, IFLCD can help with more practical problems that are hard be solved by traditional control theory.

Funder

National Natural Science Foundation of China

Publisher

American Association for the Advancement of Science (AAAS)

Subject

General Medicine

Reference27 articles.

1. Solar sail planar multireversal periodic orbits;Zeng X.;Journal of Guidance, Control, and Dynamics,2014

2. Solar sail attitude control and dynamics, part 1;Wie B.;Journal of Guidance, Control, and Dynamics,2004

3. Solar sail science mission applications and advancement;Macdonald M.;Advances in Space Research,2011

4. Propellant-efficient station-keeping using a hybrid sail in the earth-moon system;Gao C.;Nonlinear Dynamics,2019

5. Sample return from mercury and other terrestrial planets using solar sail propulsion;Hughes G. W.;Journal of Spacecraft and Rockets,2006

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