Actuator constraints handling in higher harmonic control algorithms for vibration reduction
Actuator constraints handling in higher harmonic control algorithms for vibration reduction
This paper discuses the advantages of using quadratic-programming-based higher harmonic control (HHC) algorithms for vibration reduction applications. Their benefits when dealing with actuator constraints in comparison with scaling, truncation and weight manipulation of the control efforts have been exposed in previous works. The main contribution of this work is the discussion in more detail of important implementation aspects of the quadratic programming in the context of Higher Harmonic Control. Equivalent translations of flapping constraints via constraints of the Fourier coefficients are not always possible in a quadratic-programming framework and approximations of the feasible region are required. Such approximations should be taken into consideration carefully to avoid significant loss of optimal performance. The benefits of incorporating quadratic programming algorithms in the HHC design problem are shown for a linearised representation of a five-blade coupled rotor-fuselage model augmented with active trailing edge flaps.
1094-1101
The Royal Aeronautical Society
Morales, R. M.
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Turner, M. C.
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Court, P.
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Hutchint, C.
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2014
Morales, R. M.
abe4cfe5-5e40-4e5f-bd6a-bf0f9ca4a434
Turner, M. C.
6befa01e-0045-4806-9c91-a107c53acba0
Court, P.
8b06018d-2361-4b35-9dfc-fe1020fdd9eb
Hutchint, C.
decca0ef-e216-4ba0-a180-a630b0fed6fe
Morales, R. M., Turner, M. C., Court, P. and Hutchint, C.
(2014)
Actuator constraints handling in higher harmonic control algorithms for vibration reduction.
In 40th European Rotorcraft Forum 2014.
vol. 2,
The Royal Aeronautical Society.
.
Record type:
Conference or Workshop Item
(Paper)
Abstract
This paper discuses the advantages of using quadratic-programming-based higher harmonic control (HHC) algorithms for vibration reduction applications. Their benefits when dealing with actuator constraints in comparison with scaling, truncation and weight manipulation of the control efforts have been exposed in previous works. The main contribution of this work is the discussion in more detail of important implementation aspects of the quadratic programming in the context of Higher Harmonic Control. Equivalent translations of flapping constraints via constraints of the Fourier coefficients are not always possible in a quadratic-programming framework and approximations of the feasible region are required. Such approximations should be taken into consideration carefully to avoid significant loss of optimal performance. The benefits of incorporating quadratic programming algorithms in the HHC design problem are shown for a linearised representation of a five-blade coupled rotor-fuselage model augmented with active trailing edge flaps.
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Published date: 2014
Venue - Dates:
40th European Rotorcraft Forum, ERF 2014, , Southampton, United Kingdom, 2014-09-02 - 2014-09-05
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Local EPrints ID: 439236
URI: http://eprints.soton.ac.uk/id/eprint/439236
PURE UUID: 42305cea-b951-400c-b260-d00e9b34202c
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Date deposited: 07 Apr 2020 16:31
Last modified: 18 Jan 2024 19:11
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Contributors
Author:
R. M. Morales
Author:
M. C. Turner
Author:
P. Court
Author:
C. Hutchint
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