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RPAS Satellite Communication Channel Based on IEEE 802.11b Standard

. 12–21, 2016. https://doi.org/10.18372/2306-1472.65.9815 [15] O. Kutsenko, S. Ilnytska, V. Kondratyuk and V. Konin, “Unmanned aerial vehicle position determination in GNSS landing system,” In Proceedings of the 2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD) , pp. 79–83, Kiev, Ukraine, 2017. https://doi.org/10.1109/APUAVD.2017 . [16] V. Kharchenko, V. Kondratyuk, S. Ilnytska and O. Kutsenko, “Recommendations to UAV navigation system test validation and some practical results,” In Proceedings of

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RPAS Satellite Communication Channel Based on Long-Term Evolution (LTE) Standard

–16, 2016. https://doi.org/10.18372/2306-1472.67.10426 [22] V. Kharchenko, A. Grekhov and I. Ali, “Influence of nonlinearity on aviation satellite communication channel parameters,” Proceedings of the National Aviation University , vol. 65, no. 4, pp. 12–21, 2016. https://doi.org/10.18372/2306-1472.65.9815 [23] O. Kutsenko, S. Ilnytska, V. Kondratyuk and V. Konin, “Unmanned aerial vehicle position determination in GNSS landing system,” Proceedings of the 2017 IEEE 4th International Conference Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD

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Turbine Blade of Gas Turbine Engine Additional Unloading by Changing the Layout of the Gravity Centre of the Shroud Shelf

REFERENCES [1] I. Ozoliņš, Ē. Ozoliņš and V. Fedotova, “Development of a Method for Calculating the Working Blade Stress Profile of the Aviation Gas Turbine Engine for Student Training”. Transport and Aerospace Engineering Journal . vol. 6, no. 1, pp. 55–66, 2018. https://doi.org/10.2478/tae-2018-0007 [2] A. A. Inozemcev and V. L. Sandrackij, Gazoturbinnye dvigateli . OAO Aviadvigatel. Perm, 2006. [3] R. J. Boyle, L. M. Agricola, A. H. Parikh, A. A. Ameri and V. K. Nagpal. “Shrouded CMC Rotor Blades for High Pressure Turbine Applications

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Development of a Flexible Software Solution for Controlling Unmanned Air Vehicles via the Internet

.150170 [6] N. Santos, A. Raimundo, D. Peres, P. Sebastião, and N. Souto, “Development of a software platform to control squads of unmanned vehicles in real-time,” in 2017 International Conference on Unmanned Aircraft Systems, ICUAS 2017, 2017, pp. 1-5. https://doi.org/10.1109/ICUAS.2017.7991528 [7] H. Choi, M. Geeves, B. Alsalam, and F. Gonzalez, “Open source computer-vision based guidance system for UAVs on-board decision making,” in IEEE Aerospace Conference Proceedings, 2016. https://doi.org/10.1109/AERO.2016.7500600 [8] G. Crespo, G

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Development of the Mathematical Model of Integrated Management System for an Airline

Abstract

At the present stage of airline development the most effective way to increase safety is to introduce a systematic approach to the management of the organization. The creation of a single integrated management system including the combination of resources will make it possible to maintain the necessary level of quality of aviation services with safety as a key indicator. The article offers a model of such an integrated management system for medium level airlines.

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Development of an Information Database for the Integrated Airline Management System (IAMS)

R eferences [1] R. Bogdane and V. Šestakovs, and D. Dencic, “Development of the Mathematical Model of Integrated Management System for an Airline,” Transport and Aerospace Engineering , vol. 3, pp. 44–51, 2016. ISSN 2255-9876 (online). ISSN 2255-968X (print). https://doi.org/10.1515/tae-2016-0006 [2] R. Bogdane and V. Šestakovs, “Development of mathematical model of integrated management system for an airline,” Proc. The 4th International Scientific and Practical Conference “Transport systems, logistics and engineering – 2016”, 2016, pp. 5

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Development of a Cheap Helicopter Assisted Landing System Method

Abstract

This paper presents a relatively cheap helicopter assisted landing system concept. A frequency modulated continuous radar (FMCWR) is used to check an unprepared landing area for the presence of interfering objects. The spectrum processing of the converted signal is used to provide multi target resolution. The experimental research is done by using a 4.3 GHz FMCWR radar. The converted signal spectra are provided for mirror and rough surfaces, as well for multiple targets in a case of interfering object existence.

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Evaluating the Dynamics of Aircraft Crew Skill Development by Using the Results of Discrete Exercise Marking

Abstract

Aircraft crew training corresponds to the interactive learning models of sensorimotor skill acquisition, and the dynamics of skill acquirement can be approximated by the exponential trend. A model of 5-grade assessment of separate exercises is offered. It helps to calculate a resulting evaluation, in accordance with which the progress level of a discrete exercise is evaluated. Such an evaluation forms one of the points for the analytical construction of a learning curve using the Gaussian method. Possible applications of the learning curve are covered.

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Development of a Method for Calculating the Working Blade Stress Profile of the Aviation Gas Turbine Engine for Student Training

Abstract

The paper presents a method of calculation gas turbine engine compressor or low-pressure turbine working blade profile for student training. This method of calculation was prepared for working blades with and without shroud shelves. This method provides a calculation technique to reduce the load on blade root part and the determination of blade profile stress distribution and the comparison before and after reduction of load.

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Human-In-The-Loop Remote Piloted Aerial Systems in the Environmental Monitoring

Abstract

Paper is related to development of flying robot system. The main objective is to mingle the professional backgrounds in three research directions: development of the aerial vehicle and localization, development of the tele-interaction framework and control system, development of the image fusion system and photogrammetry. Block diagrams give brief description of the systems and sub-systems under the proposed environmental system. Structure of the monitoring UAV adapted for the hand launch given.

Open access