2013
DOI: 10.1109/tmech.2013.2274558
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Hardware and Software Architecture for Nonlinear Control of Multirotor Helicopters

Abstract: Abstract-This paper presents the design and implementation of a nonlinear control scheme for multirotor helicopters that takes first-order drag effects into account explicitly. A dynamic model including the blade flapping and induced drag forces is provided and a hierarchical nonlinear controller is presented. This controller is designed for both high-precision flights as well as robustness against model uncertainties and external disturbances. This is achieved by using saturated integrators with fast desatura… Show more

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Cited by 43 publications
(21 citation statements)
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“…In order to reduce the white noise interference by using the control method of the sliding mode controller and the fuzzy reasoning mechanism, the paper analyzes the attitude analysis system by using the Lyapunov stability theory, and analyzes the attitude control of the unmanned aerial vehicle by using the control method of the unmanned aerial vehicle. The degradation of the white noise interference, and confirmed the effectiveness of the control method [57]. The Mississippi University of Science and Technology [58] uses the neural network based output feedback control for the underactuated system of the four-cantilever aircraft, using Lyapunov to track the attitude of the aircraft and effectively control the aircraft under nonlinear and bounded disturbances The University of Texas at Dallas [59].…”
Section: Software Robot Research Resultsmentioning
confidence: 76%
“…In order to reduce the white noise interference by using the control method of the sliding mode controller and the fuzzy reasoning mechanism, the paper analyzes the attitude analysis system by using the Lyapunov stability theory, and analyzes the attitude control of the unmanned aerial vehicle by using the control method of the unmanned aerial vehicle. The degradation of the white noise interference, and confirmed the effectiveness of the control method [57]. The Mississippi University of Science and Technology [58] uses the neural network based output feedback control for the underactuated system of the four-cantilever aircraft, using Lyapunov to track the attitude of the aircraft and effectively control the aircraft under nonlinear and bounded disturbances The University of Texas at Dallas [59].…”
Section: Software Robot Research Resultsmentioning
confidence: 76%
“…This symmetry allows for centralization of payload and control systems. However, their dynamic control system is highly nonlinear and very complicated and requires a highly sophisticated control techniques to control it [39,40]. Each arm contains an actuator with a fixed-pitch propeller, and its airflow goes downwards to provide lift.…”
Section: Uav Systemmentioning
confidence: 99%
“…Theoretical work has been done in understanding the dynamics of multirotor vehicles, such as quadrotors [1,2,3], hexarotors [4,5] and octorotors [6,7]. Similarly, the problem of controlling variable scaled-size helicopters has been investigated in [8], while in [9] the problem of accounting for servo actuation delay is studied.…”
Section: Related Workmentioning
confidence: 99%
“…Indicatively, it means that each 15 minutes of flight leads to the production of about 50 MB of data 4 . Thereby, the other advantage of having a fully customizable solution for data recording is that the system can be easily configured to monitor the incoming data without recording and enable/disable recording upon the recognition of a provided set of events.…”
Section: ) Data Acquisition Unitmentioning
confidence: 99%