By Amaresh Chakrabarti
This ebook showcases over 60 state of the art learn papers from the fifth foreign convention on learn into layout – the biggest in India during this region – written by means of eminent researchers from internationally on layout technique, applied sciences, tools and instruments, and their influence on innovation, for assisting layout throughout obstacles. The specified good points of the booklet are the diversity of insights into the product and approach innovation strategy, and the host of equipment and instruments from all significant parts of layout examine for the enhancement of the innovation technique. the most advantage of the booklet for researchers in a variety of components of layout and innovation are entry to the most recent caliber learn during this quarter, with the biggest selection of learn from India. For practitioners and educators, it's publicity to an empirically confirmed suite of theories, versions, tools and instruments that may be taught and practiced for design-led innovation.
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Extra resources for ICoRD’15 – Research into Design Across Boundaries Volume 2: Creativity, Sustainability, DfX, Enabling Technologies, Management and Applications
Lakshmi Narayana (&) Á G. Sharma Á G. D. Sridhara Á R. in © Springer India 2015 A. 1007/978-81-322-2229-3_2 15 16 B. Lakshmi Narayana et al. 1 Introduction A typical solar array used in satellites consists of a yoke and one or more number of panels. It is kept stowed during launch and deployed in the orbit. The yoke and panels are interconnected by hinges. The deployment of solar array is extensively tested and veriﬁed on ground before deployment in the orbit. The ground deployment testing of a solar array consisting of a yoke and two panels is shown in Fig.
Simulation as an engine of physical scene understanding. Proc. Natl. Acad. Sci. 110(45), 18327–18332 (2013) 16. : Turning pictures into numbers: extracting and generating information from complex visualizations. Int. J. Hum. Comput. Stud. 53(5), 827–850 (2000) 17. : Reconciling intuitive physics and Newtonian mechanics for colliding objects. Psychol. Rev. 120(2), 411–437 (2013) Analytical Estimation and Experimental Validation of Acceleration at Spacecraft Solar Array Latch-up Considering Differential Latching B.
The latch-up sequence of the panels influences the distribution of latch-up moments induced at the hinges. In this paper, a mathematical model for a solar array with a yoke two panel conﬁguration is developed using ADAMS software which considers differential latching of hinges. The mathematical model includes the influence of panel flexibility, close control loops, harness, snubbers, ejectors and air drag. The acceleration and moment at latch-up are estimated as a function of time. Deployment time and acceleration at latch-up dictate the magnitude of latch-up moment at hinges and have been compared with experimental value obtained from accelerometer mounted on the outermost panel, during ground deployment test.