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- W4286656367 abstract "Pitch control in fixed-wing aircraft has historically been achieved using an elevator or more recently a combination of both elevator and thrust vector control (TVC). In this research, a novel approach to achieving pitch control using a moving mass control system is proposed. The mathematical model of the moving mass in fixed-wing aircraft in the longitudinal plane is developed by modifying existing longitudinal equations of motion for aircraft. Additionally, state feedback controllers based on LQR and LQI are also developed to investigate the viability and the characteristic of the proposed moving mass pitch controller. Simulations are running for the two controllers and their step responses are analyzed. Step response with less than 15% and an improvement of more than 10 times in controllability compared to the open-loop model towards the pitch angle is achieved by both the controller." @default.
- W4286656367 created "2022-07-23" @default.
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- W4286656367 date "2022-01-01" @default.
- W4286656367 modified "2023-09-25" @default.
- W4286656367 title "Achieving Pitch Control of Fixed-Wing Aircraft Through Moving-Mass Control System" @default.
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- W4286656367 doi "https://doi.org/10.1007/978-981-19-3923-5_33" @default.
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