Aeroelastic and aeromechanical behaviour

Bramwell, A. R. S.; Done, G.T.S.; Balmford, David

doi:10.1016/b978-075065075-5/50012-9

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Dynamic Equation Of Rf-mjm1

Journal Of System Design and Dynamics1

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2014

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Cited by 2 publications

(2 citation statements)

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“…For an RFR,it is well known that C bv = 0 ,C bw = 1 2 C ω4 ω 0 (Shim (2000), Bramwell et al (2001)). Thus ,compared to the RFR,the proposed RF-MJM system will have to face the following difficulties.…”

Section: Dynamic Equation Of Rf-mjmmentioning

confidence: 99%

Modeling and Control of Rotor-Flying Multi-Joint Manipulator

Yang

Han

et al. 2014

IFAC Proceedings Volumes

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Section: Dynamic Equation Of Rf-mjmmentioning

confidence: 99%

Modeling and Control of Rotor-Flying Multi-Joint Manipulator

Yang

Han

et al. 2014

IFAC Proceedings Volumes

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“…From Refs. (2) and (11), let us consider δ ail and δ ele are the aileron and elevator control input, c and d are the flapping angles of the stabilizer bar( Fig. 5), assuming that the angular rate of the main rotor is very large in comparison with the angular rate of the fuselage.…”

Section: Journal Of System Design and Dynamicsmentioning

confidence: 99%

Nonlinear Adaptive Control for Small-Scale Helicopter

Suzuki

Nonami

2011

JSDD

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In this study, a nonlinear adaptive control system for a single-rotor type small helicopter is designed. First, a small autopilot device, which can be applied any singlerotor type helicopters, is developed based on FPGA (Field Programmable Gate Array) board. In the case of small helicopter, the payload limitation is so tight. Therefore, we can only use small and light weight sensors and computer for the control. All the sensors we use for the autopilot device are light enough to be mounted on any small helicopters. the total weight of the autopilot device with box is about 300 g. Next, a nonlinear adaptive attitude controller for small helicopter is designed by using adaptive backstepping method. It is guaranteed to make the attitude of the helicopter follows arbitrary time varying reference attitude, even when the helicopter model has the parameter uncertainties, such as inertia moment or aerodynamic uncertainties. Finally, the effectiveness of the autopilot device and the adaptive attitude controller are verified by simulation with parameter uncertainties, and the flight experiment using heterogeneous small helicopters.

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Aeroelastic and aeromechanical behaviour

Cited by 2 publications

References 9 publications

Modeling and Control of Rotor-Flying Multi-Joint Manipulator

Modeling and Control of Rotor-Flying Multi-Joint Manipulator

Nonlinear Adaptive Control for Small-Scale Helicopter

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