This manuscript deals with the detection of internal cracks and defects in aeronautical fibreglass structures. In technical practice, it is problematic to accurately determine the service life or MTBF (Mean Time Between Failure) of composite materials by the methods used in metallic materials. The problem is mainly the inhomogeneous and anisotropic structure of composites, possibly due to the differences in the macrostructure during production, production processes, etc. Diagnostic methods for detecting internal cracks and damage are slightly different, and in practice, it is more difficult to detect defects using non-destructive testing (NDT). The article deals with the use of Radio frequency identification (RFID) technology integrated in the fibreglass laminates of aircraft structures to detect internal defects based on deformation behaviour of passive RFID tag antenna. The experiments proved the potential of using RFID technology in fibreglass composite laminates when using tensile tests applied on specimens with different structural properties. Therefore, the implementation of passive RFID tags into fibreglass composite structures presents the possibilities of detecting internal cracks and structural health monitoring. The result and conclusion of the basic research is determination of the application conditions for our proposed technology in practice. Moreover, the basic research provides recommendations for the applied research in terms of the use in real composite airframe structures.

In the current world of increasing density of unmanned aerial vehicle operations in the airspace, there is an enhanced emphasis on their safety due to the potential for mid-air collision, either with another aircraft or with each other. At the same time, unmanned aerial vehicles are also being used in the context of introducing smart technologies into maintenance processes, where there is also a need to prevent a potentially possible conflict when two drones come close together. The paper introduces a mathematical model for tactical prediction of a conflict between a pair of drones. The tactical prediction of drone conflict is intended to alert the drone operator to an immediate potentially dangerous situation. The mathematical simulation in this paper extrapolates the 3D trajectory in the direction of the relative velocity vector of the convergence over the advance time. If the extrapolated trajectory has at least one point in common with the conflict space of the other drone, the conflict is signalled to the drone operator. This model can then be used in practice to simulate flight operations in shared airspace or to develop the currently required rules in selected situations.

Hand in hand with the increasing interest in the environment, this work puts the spotlight on ecological stability itself. The Coefficient of Ecological Stability (CES) indicates a chosen region’s stability level that may be calculated using various methodical instructions. For exact CES determination, it is necessary to divide the area of interest correctly into predefined classes and the division quality has a direct impact on the final CES value precision which presents its informative value. For CES calculations in the past, terrestrial measurements and processing were used. Regarding the new methods of spatial data acquisition such as photogrammetry or remote sensing, there comes the question of the usage of these data for secondary purposes, such as for ecology. This articles goal is to test the use of the images taken by an Unmanned Aerial Vehicle (UAV) for CES calculation. The main objective is to highlight the possibility of a UAV to measure CES without terrestrial measurements. The second objective is to compare the actual formulas for CES calculation and to observe the differences between the results from different calculations. Another aim is to show the inconsistency of calculations which lead to legislative unification. The aim is to apply a new method of CES calculation using Geographic Information System (GIS) software and modern methods of data acquisition and to point out the benefits, mainly including the time factor, which is closely related to the terrestrial geodetic measurement, when the CES value is about to be calculated for such a spacious area.

The rapid advancement of technology in the field of unmanned aerial vehicles (UAVs) has created new possibilities for their application in numerous fields. For every unmanned aerial system it is essential to contain a ground control station (GCS), which must comply with mission-specific requirements. This paper presents the results of our research on optimizing the hardware and software components of radio communication for an UAV prototype with hybrid propulsion and integrating them into one comprehensive control station, enabling long-range operation and universal applicability to other unmanned aircraft. Our approach includes a unique solution to separate flight control from propulsion unit monitoring due to the experimental nature of the propulsion system. Flight safety was also enhanced by equipping the GCS with a system that provides information about nearby air traffic and secures the operational area against unauthorized UAV flights. Our system is capable of detecting intruders and determining their location based on intercepting UAV radio signals. Additionally, we conducted research on radio jamming as a means of interrupting the flight of a UAV that is violating a restricted airspace. Overall, our research provides insights and recommendations for the development of effective and user-friendly GCSs for UAV systems, addressing the critical need for safe and secure UAV operations.