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Adaptive kinetic structural behavior through machine learning: Optimizing the process of kinematic transformation using artificial neural networks

Published online by Cambridge University Press:  07 October 2015

Odysseas Kontovourkis*
Affiliation:
Department of Architecture, University of Cyprus, Nicosia, Cyprus
Marios C. Phocas
Affiliation:
Department of Architecture, University of Cyprus, Nicosia, Cyprus
Ifigenia Lamprou
Affiliation:
Department of Architecture, University of Cyprus, Nicosia, Cyprus
*
Reprint requests to: Odysseas Kontovourkis, Department of Architecture, Faculty of Engineering, University of Cyprus, PO Box 20537, Nicosia 1678, Cyprus. E-mail: kontovourkis.odysseas@ucy.ac.cy
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Abstract

Nowadays, on the basis of significant work carried out, architectural adaption structures are considered to be intelligent entities, able to react to various internal or external influences. Their adaptive behavior can be examined in a digital or physical environment, generating a variety of alternative solutions or structural transformations. These are controlled through different computational approaches, ranging from interactive exploration ones, producing alternative emergent results, to automate optimization ones, resulting in acceptable fitting solutions. This paper examines the adaptive behavior of a kinetic structure, aiming to explore suitable solutions resulting in final appropriate shapes during the transformation process. A machine learning methodology that implements an artificial neural networks algorithm is integrated to the suggested structure. The latter is formed by units articulated together in a sequential composition consisting of primary soft mechanisms and secondary rigid components that are responsible for its reconfiguration and stiffness. A number of case studies that respond to unstructured environments are set as examples, to test the effectiveness of the proposed methodology to be used for handling a large number of input data and to optimize the complex and nonlinear transformation behavior of the kinetic system at the global level, as a result of the units’ local activation that influences nearby units in a chaotic and unpredictable manner.

Information

Type
Special Issue Articles
Copyright
Copyright © Cambridge University Press 2015 
Figure 0

Fig. 1. General framework for the readjustment of kinetic system by the application of control logic.

Figure 1

Fig. 2. Flowchart of the proposed kinetic structure's control mechanism toward adaptation.

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Fig. 3. Prototype unit development.

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Fig. 4. Local movement analysis.

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Fig. 5. Kinetic behavior of units at (a) primary and (b) secondary levels.

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Fig. 6. Pneumatic tube as an actuator.

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Fig. 7. Flexible pneumatic air muscle as a regulator.

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Fig. 8. Exploded prototype air manipulation.

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Fig. 9. Members connection through electromagnetic brakes.

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Fig. 10. (i) Platform at deformed level.

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Fig. 11. (ii) Platform at aligned level.

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Fig. 12. External adaptation onto a rough terrain through articulated units.

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Fig. 13. Internal adaptation through variety of configurations.

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Fig. 14. Comprehensive flowchart of the adaptive design process based on artificial neural networks (ANNs).

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Fig. 15. The architecture of artificial neural networks (ANNs) single-layer perceptron.

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Table 1. Symbols and equations of control mechanisms

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Table 2. Control mechanism's equations used

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Fig. 16. Geometrical definition and parametric control of nearby scissorlike structural units.

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Fig. 17. Digital simulation of a proposed prototype through parametric associative control.

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Fig. 18. Units alignment: (i) aligned initial state and (ii) deformed initial state.

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Table 3. Case study experiments

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Fig. 19. Units alignment: deformed initial state/deformed target state.

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Fig. 20. Average error progress in relation to training cycles (n) – L.R. 1.

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Fig. 21. Average error progress in relation to training cycles (n) – L.R. 0.1.

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Fig. 22. Error elimination progress of each unit in relation to training cycles (n) – T.P. 0.9.

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Fig. 23. Error elimination progress of each unit in relation to training cycles (n) – T.P. 0.5.

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Fig. 24. Error elimination progress of each unit in relation to training cycles (n).