Design and simulation study of novel reaction wheels with adjustable inertia for enhanced attitude control

被引：0
作者：
Keshtkar, Sajjad [1 ]
Kojima, Hirohisa [1 ]
机构：
[1] Tokyo Metropolitan Univ, Dept Aeronaut & Astronaut, 6-6 Asahigaoka, Hino, Tokyo 1910065, Japan
来源：
MECHANISM AND MACHINE THEORY | 2024年 / 197卷
关键词：
Attitude control; Deployable mechanisms; Reaction wheels; Variable geometry mechanisms; FLYWHEEL; DESATURATION;
D O I：
10.1016/j.mechmachtheory.2024.105636
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
This study introduces a novel approach for improving the performance of reaction wheels by dynamically altering their moment of inertia. To achieve this, several innovative mechanisms based on adjustable mass distribution, wheels with variable geometry, and systems with multiple wheels are proposed. A generalized mathematical model is developed, which employs the radius of gyration as the variable. Detailed 3D designs of these concepts are introduced, and their characteristics, theoretical behavior, and potential performance are explored through mathematical modeling and simulations. The study also emphasizes the efficiency of these systems in attitude control, by analyzing their dynamic behavior under various control strategies.
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页数：15
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