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ELECTRIC BUSES it is possible to define the additional charging time at the terminus for unitary distance of transportation route [min/km]: (5.12) The cumulative distribution of additional charging time was calculated for the following variants: - Pch-m = 70 kW, Pch-s = 70 kW, l"=0,3, - Pch-m = 200 kW, Pch-s = 50 kW, l"=0,15, - Pch-m = 250 kW, Pch-s = 70 kW, l"=0,1. Results of the calculation are shown on fig. 5.5 - 5.10. Fig. 5.5. The cumulative distribution of successful charging probability in function of

: 2.02.2017]. [23] http://www.eutelsat.com/en/home.html [access: 2.02.2017]. [24] Messier D., 2011, „Will a new space power rise along the Atlantic?”, The Space Review, 15.08.2011., http://www.thespacereview.com/article/2143/1 [access: 10.03.2017]. [25] https://www.kyivpost.com/article/content/ukraine-politics/first-launch-of-ukrainian-brazilianrocket-schedul-114278.html [access: 10.03.2017]. [26] http://ilot.edu.pl/wspolpraca/partnerzy-zagraniczni/uniwersytet-w-brasilii/ [access: 4.07.2017]. [27] Gocłowska-Bolek J., 2017, „Ameryka Łacińska w poszukiwaniu

2014-2019” Lotnictwo nr 3/2014 Magazyn miłośników lotnictwa wojskowego, cywilnego i kosmonautyki Wydawca Magnum X Sp. zo.o, Warszawa. [25] Müller H. Stolár M., 2006, “Siły Powietrzne Chorwacji” Przetłumaczył: Andrzej Kiński Lotnictwo nr 6/2006 Magazyn miłośników lotnictwa wojskowego, cywilnego i kosmonautyki Wydawca Magnum X Sp. zo.o, Warszawa. [26] “MiG-21 tylko dla doświadczonych pilotów, 2012, Przegląd Sił Powietrznych nr 03 (60) Kwartalnik, – przedruk 14 S. Hobson: Canada builds a future with equipment and experience gained in Afghanistan. “Jane’s International

. Using the same value of the control parameter as before, i.e. =0.03, we see now that the highest velocity drops to 0.56V  and the lowest to V = 0.38. This time, the solution (to be precise the “sub-solution”) consists of 25 cycles that form a sequence of three and two impacts per period of the limiter motion (see Fig. 5.13 and Fig. 5.14). 5.1. Sawtooth Wave Limiter 116 Figure 5.12. Bifurcation diagram for µ=0.5 Figure 5.13. Drift of twenty five-cycle solution Let us summarise the above comparison of three cases of a dynamic system possessing the