The parameters optimisation design for variable speed control momentum gyroscopes
Control momentum gyroscopes (CMGs) have many advantages over other actuators for the attitude control of a spacecraft. Compared with the single-gimbal control moment gyroscopes (SGCMGs), the mass and power of the flywheel of variable-speed control moment gyroscopes (VSCMGs) are greatly increased. In...
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| Vydané v: | International journal of control Ročník 90; číslo 12; s. 2618 |
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| Jazyk: | English |
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Abingdon
Taylor & Francis Ltd
01.12.2017
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| Abstract | Control momentum gyroscopes (CMGs) have many advantages over other actuators for the attitude control of a spacecraft. Compared with the single-gimbal control moment gyroscopes (SGCMGs), the mass and power of the flywheel of variable-speed control moment gyroscopes (VSCMGs) are greatly increased. In this paper, a new solving strategy of singularity problem is proposed, which concludes the exchangeable momentum and steering law, and the parameters of VSCMGs are designed based on the constraint of singular problem. The configuration characteristics of VSCMGs with the constraint of upper and lower bounds of the flywheel regulation speed are revealed. The steering characteristics of weighted pseudo-inverse with null motion (WPINM) are analysed, then the flywheel torque requirement of WPINM is evaluated based on the geometry theory. At last, the parameter design problem of VSCMGs is cast as multi-objectives and bi-level programming problem. The bi-level programming is transformed into a single-level programming problem by using of the Karush-Kuhn-Tucker condition. Finally, the intelligent algorithm of particle swarm optimisation is presented to solve the nonlinear multi-objective problem. |
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| AbstractList | Control momentum gyroscopes (CMGs) have many advantages over other actuators for the attitude control of a spacecraft. Compared with the single-gimbal control moment gyroscopes (SGCMGs), the mass and power of the flywheel of variable-speed control moment gyroscopes (VSCMGs) are greatly increased. In this paper, a new solving strategy of singularity problem is proposed, which concludes the exchangeable momentum and steering law, and the parameters of VSCMGs are designed based on the constraint of singular problem. The configuration characteristics of VSCMGs with the constraint of upper and lower bounds of the flywheel regulation speed are revealed. The steering characteristics of weighted pseudo-inverse with null motion (WPINM) are analysed, then the flywheel torque requirement of WPINM is evaluated based on the geometry theory. At last, the parameter design problem of VSCMGs is cast as multi-objectives and bi-level programming problem. The bi-level programming is transformed into a single-level programming problem by using of the Karush-Kuhn-Tucker condition. Finally, the intelligent algorithm of particle swarm optimisation is presented to solve the nonlinear multi-objective problem. |
| Author | Wang, Long Liu, Feng Guo, Yang Yao, Yu Zhao, Hui |
| Author_xml | – sequence: 1 givenname: Feng surname: Liu fullname: Liu, Feng – sequence: 2 givenname: Hui surname: Zhao fullname: Zhao, Hui – sequence: 3 givenname: Yu surname: Yao fullname: Yao, Yu – sequence: 4 givenname: Yang surname: Guo fullname: Guo, Yang – sequence: 5 givenname: Long surname: Wang fullname: Wang, Long |
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| Snippet | Control momentum gyroscopes (CMGs) have many advantages over other actuators for the attitude control of a spacecraft. Compared with the single-gimbal control... |
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| SubjectTerms | Control moment gyroscopes Design optimization Design parameters Flywheels Gyroscopes Laws Lower bounds Multiple objective analysis Product design Programming Spacecraft attitude control Speed control Steering |
| Title | The parameters optimisation design for variable speed control momentum gyroscopes |
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