**6. Conclusions**

The results from simulation help to overcome the physical and architectural limitations of computational power that can be achieved with a single-processor system. It is then very convenient for the application to use a more powerful processor, a faster cache, and faster access to the RAM with higher transfer capacity. The results obtained in the simulation of structured mathematical models of aircraft motion and the use of this method appear to be effective and pragmatic according to the requirements of the integration algorithm given in the chapter.

In general, in accordance with the proposed solution, it is also possible to run the program faster due to factors such as the availability of better bandwidth for communication within node. Greater bandwidth provides additional communication with the interface to transfer message between nodes and the higher performance of the graphics processing unit.

The described design of a structured mathematical model of aircraft motion to perform simulation on the GPU, this simulation was chosen as an example of an algorithm confirming the proposed solution. The presented problem of simulation methods of block structure of mathematical models of aircraft motion was solved by predetermined known procedures. The advantages of the methods are a combination of both the features: the efficiency of computer system programming and the scalability of a GPU computational method.

Based on knowledge gained in design of the block structure of mathematical models of aircraft motion, we can say that the graphics card can be used in multiple and parallel simulation, which confirms high speed of computations. The advantage of faster simulation can sometimes be obtained at the earliest defined quality. These facts and accuracies are well suited for use in real-time simulation and a virtual reality imaging system. The results of the simulation of such designed structured mathematical model of aircraft motion show very fast calculation and confirm the effectiveness of such a structure of the mathematical model of aircraft for the proposed system of the simulator, which was the motivation of our research.
