Simulation analysis of a flight control law with in-flight performance optimization

Gurbuz Taha Ozdemir, Joseph F. Horn

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

16 Citations (Scopus)

Abstract

A flight control system is designed to perform in-flight optimization of redundant control effectors on a rotorcraft in order to minimize power required at a given flight condition. This "Fly to Optimal" (FTO) control law is tested in simulation using the GENHEL model of the UH-60A and a compound version of the UH-60 with lifting wing and vectored thrust ducted propeller (VTDP). A model following controller is implemented for the pitch, roll, yaw, heave and rotor RPM axes. An outer loop is designed to control forward and sideward translational rate and hold airspeed and altitude during optimization. Two approaches were used to perform in-flight optimizations. A Golden Section search method was used to find optimal rotor RPM on a conventional helicopter, where the single redundant control effector is rotor RPM. A method based on the Adaptive Performance Optimization (APO) methods was used to optimize trim on a compound rotorcraft with several redundant control effectors. The controller can be used to optimize rotor RPM and compound control effectors through flight test or simulations in order to establish a schedule. Alternatively, in-flight optimizations can be performed in level flight cruise conditions without altering flight conditions significantly. Simulation results show the FTO method to be effective in reaching optimal, although in some cases requiring relatively long period of simulated flight time.

Original languageEnglish (US)
Title of host publication68th American Helicopter Society International Annual Forum 2012
Pages2106-2117
Number of pages12
StatePublished - Aug 17 2012
Event68th American Helicopter Society International Annual Forum 2012 - Fort Worth, TX, United States
Duration: May 1 2012May 3 2012

Publication series

NameAnnual Forum Proceedings - AHS International
Volume3
ISSN (Print)1552-2938

Other

Other68th American Helicopter Society International Annual Forum 2012
CountryUnited States
CityFort Worth, TX
Period5/1/125/3/12

Fingerprint

Flight dynamics
Rotors
Controllers
Flight control systems
Propellers
Helicopters

All Science Journal Classification (ASJC) codes

  • Engineering(all)

Cite this

Ozdemir, G. T., & Horn, J. F. (2012). Simulation analysis of a flight control law with in-flight performance optimization. In 68th American Helicopter Society International Annual Forum 2012 (pp. 2106-2117). (Annual Forum Proceedings - AHS International; Vol. 3).
Ozdemir, Gurbuz Taha ; Horn, Joseph F. / Simulation analysis of a flight control law with in-flight performance optimization. 68th American Helicopter Society International Annual Forum 2012. 2012. pp. 2106-2117 (Annual Forum Proceedings - AHS International).
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Ozdemir, GT & Horn, JF 2012, Simulation analysis of a flight control law with in-flight performance optimization. in 68th American Helicopter Society International Annual Forum 2012. Annual Forum Proceedings - AHS International, vol. 3, pp. 2106-2117, 68th American Helicopter Society International Annual Forum 2012, Fort Worth, TX, United States, 5/1/12.

Simulation analysis of a flight control law with in-flight performance optimization. / Ozdemir, Gurbuz Taha; Horn, Joseph F.

68th American Helicopter Society International Annual Forum 2012. 2012. p. 2106-2117 (Annual Forum Proceedings - AHS International; Vol. 3).

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

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Ozdemir GT, Horn JF. Simulation analysis of a flight control law with in-flight performance optimization. In 68th American Helicopter Society International Annual Forum 2012. 2012. p. 2106-2117. (Annual Forum Proceedings - AHS International).