We test the influence of control using classic configuration control variables and pusher propeller control variables on the obtained speed and other parameters. – Currently, the tests focus on accelerating the helicopter to the set flight speed, while maintaining the set values of other helicopter state variables, such as flight altitude. – Our system integrates two control methods to provide the desired helicopter responses - explains Sebastian Topczewski, PhD, Eng. In this way, they want to verify whether it is possible to achieve the desired speed in forward flight, while maintaining flight safety. They check how different control modes affect the performance of the helicopter. Not only do they develop an automatic control system, but they also test it. (aviation and aerospace students specializing in automation and aviation systems) together with Sebastian Topczewski, PhD, Eng., conduct their research at the Division of Automation and Aeronautical Systems of the Faculty of Power and Aeronautical Engineering.
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It is worth noting that the works are carried out as part of a series of grants sponsored by Boeing, with the invaluable support of the company's manager – Szymon Trąbała. In addition to technical issues, they learn and implement good practices of agile project management. – Students deepen their knowledge in the field of helicopter movement modelling and automatic control methods. – This is a grant intended for students and it is they who carry out most of the works planned to be done – says Sebastian Topczewski, PhD, Eng. Today, the effects of that work are of benefit to new group. together with a group of students was at that time engaged in the development of a reconfigurable, compound unmanned helicopter. This helicopter was created as part of another project run at the Faculty of Power and Aeronautical Engineering.
In their research, the WUT team uses a fully functional helicopter and its validated numerical model, developed in the FLIGHTLAB environment. Our team strives to develop effective solutions in the field of automatic control, making it possible to achieve high cruising speeds while maintaining flight safety. The assumption of such a configuration is that the helicopter achieves a higher forward flight speed. – In relation to the classic configuration of the helicopter (the main rotor and the tail rotor), we include an additional pusher propeller, located at the end of the tail boom. – We are developing an automatic flight control system enabling the implementation of the defined missions – explains Sebastian Topczewski, PhD, Eng. And it is exactly what WUT students and employees are working on! EMAT was established in reponse to recommendations to create a fly-in team to enhance reponses to natural distasters and other emergencies. Due to additional control variables, automation of control becomes crucial here.
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Logitech X52 Pro Flight Control System (PC) (8) 296.07. As a result, these machines have extensive control systems. Browse deals on Joysticks & Flight Controllers, Gaming Panels, Gaming Pedals, Gaming Throttles. by adding an additional pusher propeller. However, these configurations are more complex than classic helicopters, e.g.
Increased forward speeds and greater range means that compound helicopters are perceived as the future of the industry.
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