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

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 2 . 9 % for a 3 . 6 m 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 500 μ m for a period of 15 min corresponded to 4 . 6 % for the 3 . 6 m long truss.

[1]  Michael E. McEachen Verification of Deployment Precision and Stability Requirements for the GEMS Telescope Optical Boom , 2013 .

[2]  Hiroshi Furuya,et al.  Variable geometry truss and its application to deployable truss and space crane arm , 1985 .

[3]  Lee D. Peterson,et al.  Submicron Mechanical Stability of a Prototype Deployable Space Telescope Support Structure , 1999 .

[4]  Wei Dong,et al.  A Piezo-Actuated High-Precision Flexible Parallel Pointing Mechanism: Conceptual Design, Development, and Experiments , 2014, IEEE Transactions on Robotics.

[5]  Lawrence F. Rowell,et al.  Thermal-distortion analysis of a spacecraft box truss in geostationary orbit , 1990 .

[6]  Koryo Miura,et al.  Adaptive Structures Research at ISAS, 1984-1990 , 1992 .

[7]  Yung Ting,et al.  Error compensation and feedforward controller design for a 6-dof micro-positioning platform , 2005, 2005 IEEE/RSJ International Conference on Intelligent Robots and Systems.

[8]  W. Keith Belvin,et al.  Advances in Structures for Large Space Systems , 2004 .

[9]  Sergio Pellegrino,et al.  Shape Accuracy of a Joint-Dominated Deployable Mast , 2010 .

[10]  E. Crawley,et al.  Adaptive Structures , 1990 .

[11]  Hiroshi Furuya,et al.  Prediction, measurement and stabilization of structural deformation on orbit , 2010 .

[12]  K. Minesugi,et al.  A technique to evaluate on-orbit thermal deformation for large precise structures in ASTRO-H , 2015 .

[13]  D. Stewart A Platform with Six Degrees of Freedom , 1965 .

[14]  J. Mahaney,et al.  Fundamental studies of thermal-structural effects on orbiting trusses , 1982 .

[15]  Benjamin K. Henderson,et al.  Recent achievements and new opportunities in adaptive structures , 2001 .