A model following controller optimized for gust rejection during shipboard operations

Joseph F. Horn, Derek O. Bridges

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

23 Scopus citations

Abstract

A flight control design methodology for reducing pilot workload during shipboard operation of helicopters is presented. The objective of the control synthesis is to improve the gust rejection properties of the aircraft when operating in an unsteady ship airwake. An airwake compensator is designed to integrate with a standard model following control scheme. The spectral properties of the ship airwake are used in the design of the airwake compensator. The model following controller and airwake compensator are implemented in a simulation model of a UH-60A Black Hawk operating near an LHA-class ship. Simulations were performed for approaches and hovering over the deck. The results show that the airwake compensator results in significantly lower angular motion of the aircraft when compared to a basic model following controller without the airwake compensator.

Original languageEnglish (US)
Title of host publicationAHS International 63rd Annual Forum - Proceedings - Riding the Wave of New Vertical Flight Technology
Pages1078-1111
Number of pages34
StatePublished - 2007
Event63rd American Helicopter Society International Annual Forum 2007 - Virginia Beach, VA, United States
Duration: May 1 2007May 3 2007

Publication series

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

Other

Other63rd American Helicopter Society International Annual Forum 2007
Country/TerritoryUnited States
CityVirginia Beach, VA
Period5/1/075/3/07

All Science Journal Classification (ASJC) codes

  • General Engineering

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