An Unmanned Aerial Vehicle (UAV) is referred to as a remotely piloted aircraft or an unmanned aircraft which can be navigated with human operator in the loop. This paper discusses the design of a UAV with Vertical Take-Off and Landing (VTOL) capability for Maritime applications. The design provides a means for surveillance and communication in Maritime applications. The VTOL-UAV utilises a five-rotor propulsion system that can be launched from confined platforms such as ship-decks. The intended applications of this M-UAV drove the development of an innovative landing system which in the case of emergencies can allow the M-UAV’s soft and potential landing on the water surface. The other functionalities of this UAV are its capabilities to deploy communication Micro-sonobuoys which allows for communication with underwater Robot(s) via Operator in the loop. In this paper we also discuss the process of structural design modelling and evaluation of the development of the Maritime Unmanned Air Vehicle.
It sets up the system structure model of materiel system reliability simulation based on Adaptive Agent in the paper, emphasizes the mission-oriented reliability impact model and the devising thinking on MA, which helps to mission environment-oriented reliability analysis.
Scene simulation technology has been developed into a research focus with the military simulation development. The key technologies of the scene simulation federate are discussed in this paper, and then the method of integration between HLA and Vega, and the way of keeping the integrality of scene simulation information are presented. This article outlines the development process of the scene simulation federate of plane's Reliability, Maintainability and Supportability (RMS) requirement determination simulation system based on HLA, Vega and Visual C++. The scheme of scene simulation federate is helpful for the development of similar equipment's scene simulation. The simulation results indicate that the scene simulation federate can vividly image the actual use of plane, achieve the expected functions and effects and improve the effects of plane's RMS requirement determination.
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