Optimization of a helicopter stability augmentation system for operation in a ship airwake

Dooyong Lee, Joseph F. Horn

Research output: Chapter in Book/Report/Conference proceedingConference contribution

10 Citations (Scopus)

Abstract

A stability augmentation system is optimized for a UH-60 helicopter operating in a turbulent ship airwake. The system is demonstrated using a flight dynamic model based on the GENHEL software integrated with CFD solutions of the airwake of a LHA ship. A stochastic airwake model was developed for more efficient simulation and analysis. The stochastic model uses an equivalent six-component gust vector and shaping filters based on the von Karman turbulence model. The filters were derived from simulations of the helicopter with full time-varying CFD airwake solutions. The proposed stochastic airwake model can be easily integrated with off-line analysis or real-time applications. For disturbance rejection, a new performance specification is designed based on the power spectrum density of the transfer function between the gust inputs and aircraft rate responses. The baseline limited authority SAS is modified and optimized using CONDUIT® (Control Designer's Unified Interface) in order to improve handling-qualities and stability, and to minimize a weighted objective of gust responses. The optimized SAS are tested using the non-linear simulation model with time-varying airwake. Time domain and frequency domain analyses of the simulation show that the modified SAS resulted in reduction of pilot workload in the longitudinal and directional axes, with modest improvements in the lateral axis.

Original languageEnglish (US)
Title of host publication61st Annual Forum Proceedings - AHS International
Pages1284-1294
Number of pages11
StatePublished - Dec 1 2005
Event61st American Helicopter Society International Annual Forum 2005 - Grapevine, TX, United States
Duration: Jun 1 2005Jun 3 2005

Publication series

NameAnnual Forum Proceedings - AHS International
Volume2
ISSN (Print)1552-2938

Other

Other61st American Helicopter Society International Annual Forum 2005
CountryUnited States
CityGrapevine, TX
Period6/1/056/3/05

Fingerprint

Stochastic models
System stability
Helicopters
Ships
Computational fluid dynamics
Flight dynamics
Disturbance rejection
Power spectrum
Turbulence models
Transfer functions
Dynamic models
Aircraft
Specifications

All Science Journal Classification (ASJC) codes

  • Engineering(all)

Cite this

Lee, D., & Horn, J. F. (2005). Optimization of a helicopter stability augmentation system for operation in a ship airwake. In 61st Annual Forum Proceedings - AHS International (pp. 1284-1294). (Annual Forum Proceedings - AHS International; Vol. 2).
Lee, Dooyong ; Horn, Joseph F. / Optimization of a helicopter stability augmentation system for operation in a ship airwake. 61st Annual Forum Proceedings - AHS International. 2005. pp. 1284-1294 (Annual Forum Proceedings - AHS International).
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Lee, D & Horn, JF 2005, Optimization of a helicopter stability augmentation system for operation in a ship airwake. in 61st Annual Forum Proceedings - AHS International. Annual Forum Proceedings - AHS International, vol. 2, pp. 1284-1294, 61st American Helicopter Society International Annual Forum 2005, Grapevine, TX, United States, 6/1/05.

Optimization of a helicopter stability augmentation system for operation in a ship airwake. / Lee, Dooyong; Horn, Joseph F.

61st Annual Forum Proceedings - AHS International. 2005. p. 1284-1294 (Annual Forum Proceedings - AHS International; Vol. 2).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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Lee D, Horn JF. Optimization of a helicopter stability augmentation system for operation in a ship airwake. In 61st Annual Forum Proceedings - AHS International. 2005. p. 1284-1294. (Annual Forum Proceedings - AHS International).