By Adrien Champion, Rémi Delmas (auth.), Charles Pecheur, Michael Dierkes (eds.)
This booklet constitutes the completely refereed convention complaints of the 18th overseas Workshop on Formal equipment for commercial serious structures, FMICS 2013, held in Madrid, Spain, in September 2013. The thirteen papers provided have been conscientiously chosen from 25 submissions and canopy subject matters reminiscent of layout, specification, code iteration and checking out in accordance with formal equipment, equipment, options and instruments to help computerized research, certification, debugging, studying, optimization and transformation of complicated, disbursed, liable, real-time structures and embedded structures, verification and validation equipment, instruments for the advance of formal layout descriptions, case experiences and adventure studies on commercial functions of formal tools, influence of the adoption of formal equipment at the improvement technique and linked bills, program of formal tools in standardization and commercial forums.
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Additional info for Formal Methods for Industrial Critical Systems: 18th International Workshop, FMICS 2013, Madrid, Spain, September 23-24, 2013. Proceedings
We consider a simpliﬁed model of an unmanned aerial vehicle, such as a helicopter or an airplane, where we only treat the vertical position h and vertical velocity v of the system. e. with gravitational acceleration g = −10m/s2, from crashing into the ground, h = 0. This is done by accelerating the vehicle upwards with acceleration auav = 20m/s2 , when the height reaches a certain minimal value h = 1m. We only consider values in the range 0 − 4m for height, and −12 to 12m/s for velocity. In Figure 1-(b) we give a graphical illustration of a hybrid automaton Huav modeling the system described above with initial velocity v0 and position h0 .
The work-ﬂow is being evaluated in the context of case studies. The primary case study is that of the application software for an automatic transmission controller. However, the majority of the experiences described in this paper so far Workﬂow for Practical Formal Veriﬁcation 35 relate to a smaller case study related to the control of a basic hydraulic system1 . We have started with the smaller case-study to provide a simpler learning environment as we gain experience in the work-ﬂow. The next section looks at these veriﬁcation activities, and discusses the potential beneﬁts, approach adopted, prerequisites and limitations.
The initial states Init are all in location lfree , with c = 0. Since we are interested in backwards reachability analysis of hybrid automata we will in the following let the term linear emergency control automaton refer to the reverse of the automata given by Deﬁnition 8. In Figure 2 we give an graphical overview of the characteristics of a general (reverse) linear emergency control automaton, namely that the transition from the reverse linear emergency control to the lfree location can be taken at any time but never left, and that the run stops when the clock c, initially tfree , reaches 0.