Fundamental performance of a smart structural system utilizing thermal expansion for pointing

Author:

Shimada Takeshi1,Ishimura Kosei2,Taro Kawano3

Affiliation:

1. Department of Aeronautics and Astronautics, School of Engineering, The University of Tokyo, Tokyo, Japan

2. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Tokyo, Japan

3. Japan Aerospace Exploration Agency, Tokyo, Japan

Abstract

This study involved designing and developing a smart structural system for pointing control of large-scale trusses. The system consisted of a pointing control mechanism, an internal displacement-sensor, and a controller. The significant points of the system included the following: (1) artificial thermal expansions of truss members were utilized as linear actuators, (2) elastic hinges were employed instead of ball joints, and (3) the internal displacement-sensor that did not require external jigs and possessed high measuring accuracy was applied. The study involved conducting a feasibility study and an experimental demonstration. The results indicated that the pointing control mechanism produced a sufficient tilt angle to satisfy typical requirements of recent scientific satellites. Furthermore, the findings confirmed that the hysteresis of the pointing control mechanism could be kept sufficiently small due to the absence of sliding parts. The difference between the finite element analysis and the measured value corresponded to [Formula: see text] for a [Formula: see text] long truss. Additionally, the results suggested that the proposed smart structural system for pointing exhibited high control accuracy and tracking performance for a periodic motion. The root mean square error value for a circular trajectory with a radius of [Formula: see text] for a period of [Formula: see text] corresponded to [Formula: see text] for the [Formula: see text] long truss.

Publisher

SAGE Publications

Subject

Mechanical Engineering,General Materials Science

Reference15 articles.

1. Advances in Structures for Large Space Systems

2. Cosgrove PA, Farmer JT, Rowell LF (1990) Thermal-distortion analysis of a spacecraft box truss in geostationary orbit. NASA Technical Reports, Report no. H/118 0303184, Washington, DC: National Aeronautics and Space Administration, pp. 1–26.

3. Recent achievements and new opportunities in adaptive structures

4. A Piezo-Actuated High-Precision Flexible Parallel Pointing Mechanism: Conceptual Design, Development, and Experiments

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