Continual Monitoring of Precision of Aerial Transport Objects
暂无分享,去创建一个
In accordance with the future aims, when these aerial transport objects (ATO) could fly in a selected corridor, it is also important to simulate states based on the status monitoring of dangerous situated in the complex environmental condition of the Slovak Republic (SR). With due regard to the orography of the territory, it is important to locate residual areas, where there is no possibility of their telemetric control. In the given issue, however, it is also necessary to take into account the legal framework representing a supplementary control function of maintaining flight safety of air traffic control in compliance with the ATM policies. The set-up of functional efficiency of controlling the flight of such an ATO in a complex area must be stable. In the article, stability is presented by error analysis at given lateral deviations after the ATO has switched into autonomous flight mode. Due to the errors caused by the external environment, the ATO must perform a precise flight into the area and achieve the success of the flight mission. For example, it may involve a flight into mountain territories, where it is important to secure the patient s status or the person under threat. The laboriousness of solution of such flights in a limited mountain terrain is divided into files of intelligent autonomous ports (Sky Control Object Power Environment – SCOPE). The task is to cover the residual areas for minimizing the time of rescuing persons present in the active corridors taking into account the probability of environmental change. Analysis in the article is the fundamental navigational task of flying in the corridor itself in a precise navigation mode of autonomous flight, while presuming the possibility of error occurrence of the Navigation Ergatic Complex (NEC), the element of which are made up of an inertial navigation system, Doppler sensor of speed and drift angle carried on an unmanned aerial vehicle.
[1] Peter Korba. UNMANNED HELICOPTER TAIL UNIT FEM ANALYSIS , 2017 .
[2] Rudolf Andoga,et al. Integration architecture design for implementation of a vector magnetometer on board of unmanned vehicle , 2014, 2014 IEEE 15th International Symposium on Computational Intelligence and Informatics (CINTI).
[4] Jozef Kozar,et al. Geometric dilution of precision of the GNSS for Mars (GNSS FATIMA) , 2016 .