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[Studies in Computational Intelligence 481] Artur Babiarz, Robert Bieda, Karol Jędrasiak, Aleksander Nawrat (auth.), Aleksander Nawrat, Zygmunt Kuś (eds.) - Vision Based Systemsfor UAV Applications (2013, Sprin

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200 D. Cedrych et al.<br />

Table 1. Indices values of <strong>UAV</strong> path for <br />

Simulation number <br />

1 2722 3602 800<br />

2 3900 4983 1500<br />

3 3293 4241 1150<br />

4 3530 4616 1300<br />

5 3140 3761 800<br />

Average value 3317 4240 1100<br />

Table 2. Indices values of <strong>UAV</strong> path for <br />

Simulation number <br />

1 2791 3187 750<br />

2 3743 4170 850<br />

3 2574 3021 750<br />

4 3131 3921 950<br />

5 2991 3381 750<br />

Average value 3046 3536 810<br />

Table 3. Indices values of <strong>UAV</strong> path for <br />

Simulation number <br />

1 3219 3500 750<br />

2 2700 3057 750<br />

3 2661 2837 550<br />

4 3055 3491 650<br />

5 3054 2520 950<br />

Average value 2937.8 3281 730<br />

4 Conclusions<br />

In this chapter set of simulations that generates solution of the problem of collision<br />

free path plann<strong>in</strong>g <strong>in</strong> 3D space was presented. The target application of the<br />

discussed method is determ<strong>in</strong>ation of the way po<strong>in</strong>ts of the flight of the <strong>UAV</strong>.<br />

Presented approach allows to f<strong>in</strong>d feasible path <strong>in</strong> 3D space simultaneously reduc<strong>in</strong>g<br />

the computations. Thanks to the simplification that consists <strong>in</strong> splitt<strong>in</strong>g the<br />

process on two stages the method is both effective and simple (<strong>in</strong> terms of computation<br />

costs). The simplicity was the one of the most important assumptions taken<br />

for the design of the <strong>UAV</strong> control system. S<strong>in</strong>ce the method is not determ<strong>in</strong>istic it<br />

generates different solutions. After a number of simulations it was checked that all<br />

the generated solutions are also feasible ones and they are satisfactory for the<br />

overall <strong>UAV</strong> control system.

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