![]() ![]() Furthermore, as the major airline players increase the size of their fleets, the demand for technologically better flight control computers for future aircraft will increase. ![]() Manufacturers of aircraft flight control systems are creating advanced components that will lower total aircraft weight while enhancing overall efficiency, influencing market growth for aircraft flight control computers. Additionally, the increased air traffic footprint is expected to influence the demand for commercial aircraft globally.įlight Control Computers is expected to account for the largest share in 2022.īased on Component, the flight control computers segment is projected to lead the aircraft flight control systems market during the forecast period. The anticipated rise in demand for commercial aircraft and the rising use of lightweight flight control systems to fulfill the demand for modern aircraft. The Aircraft Flight Control Systems market size is projected to grow from USD 14.5 Billion in 2022 to USD 21.5 Billion by 2027, at a CAGR of 8.2 % from 2022 to 2027. 15, 2022 (GLOBE NEWSWIRE) - The "Aircraft Flight Control Systems Market by Component (Cockpit Controls, Flight Control Computer, Actuators, Sensors), Platform (Commercial Aviation, Military Aviation, Business & General Aviation), Fit, Technology and Region - Global Forecast to 2027" report has been added to 's offering. The integrated design methodology has been developed in the context of the H2020 STRATOFLY Project and it has been exploited for the design and sizing of the Flight Control System of the STRATOFLY MR3 vehicle, a Mach 8 waverider concept for civil antipodal flights.Dublin, Nov. Eventually, the Flight Control System design is completed with the selection of actuators and finalization of the System architecture including power distribution lines and connections with the avionic system. A novel approach is here suggested to extend the formulation available in literature beyond the transonic regime. Maximum required control surfaces deflections are used as inputs for the estimation of hinge moments to be counteract by the actuation system. ![]() Indeed, in order to minimize the exploitation of control surfaces and thus limiting the detrimental effects onto the aerodynamic efficiency, propellant tanks can be properly shaped and integrated on board, and ad-hoc depletion sequencies can be adopted to match the desired center of gravity shift throughout the mission. At this stage, the interaction with the propellant system is fundamental to identify the minimum surfaces deflections required to guarantee the aircraft trim. The newly defined surfaces can be analyzed to predict their single contribution to the vehicle lift and drag coefficients. The integrated subsystems design methodology disclosed in this paper starts with the suggestion of the most promising semi-empirical models for control surfaces geometrical definition. Therefore, this paper discloses an innovative methodology (i) to anticipate the Flight Control System design of future high-speed aircraft at conceptual design stage, (ii) to properly consider the interactions with other subsystems and (iii) to properly predict the behavior of the Flight Control System throughout the entire mission. Conversely, typical supersonic and hypersonic design solutions are investigated by means of numerical simulations which guarantee higher accuracy but may not be directly applicable during the early design stages. On the other side, traditional design approaches widely used in subsonic aircraft design and based on on-design and standalone system sizing, may lead to wrong estimates of the peak power demand. On one side, a preliminary characterization of the control surfaces is essential for a precise estimate of the aerodynamic characteristics of the vehicle throughout the mission. Flight Control System is considered a key enabler for future high-speed aircraft and therefore, the anticipation of its impact onto the aircraft layout and performance is crucial. ![]()
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