Robust LPV H gain-scheduled hover-to-cruise conversion for a tilt-wing rotorcraft in the presence of CG variations

Jeffrey J. Dickeson, David Miles, Oguzhan Cifdaloz, Valana Wells, Armando Rodriguez

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

18 Citations (Scopus)

Abstract

This paper describes the development and analysis of gain-scheduled, multi-variable H∞ control law for the conversion of a linear parameter varying (LPV) model of a High-Speed Autonomous Rotorcraft Vehicle (HARVee), an experimental tilt-wing aircraft. Tilt-wing aircraft combine the high-speed cruise capabilities of a conventional airplane with the vertical takeoff and station keeping abilities of a helicopter by rotating their wings at the fuselage. Changing between cruise and hover flight modes in mid-air is referred to as the conversion process, or simply conversion. A nonlinear aerodynamic model was previously developed that captures the unique dynamics of the tilt-wing aircraft. An H∞ design methodology was used to develop linear controllers along various operating points of a conversion trajectory. The development of these control systems was governed not only by performance specifications at each particular operating point, but also by the unique requirements of a gain-scheduled conversion control system. The performance of the resulting conversion closed-loop systems is analyzed in the frequency and time domains. Performance robustness with respect to variation in the location of the center of gravity (eg) has been studied.

Original languageEnglish (US)
Title of host publicationProceedings of the IEEE Conference on Decision and Control
Pages2773-2778
Number of pages6
DOIs
StatePublished - 2007
Event46th IEEE Conference on Decision and Control 2007, CDC - New Orleans, LA, United States
Duration: Dec 12 2007Dec 14 2007

Other

Other46th IEEE Conference on Decision and Control 2007, CDC
CountryUnited States
CityNew Orleans, LA
Period12/12/0712/14/07

Fingerprint

Control systems
Fuselages
Takeoff
Closed loop systems
Helicopters
Aerodynamics
Gravitation
Trajectories
Aircraft
Specifications
Controllers
Air

ASJC Scopus subject areas

  • Control and Systems Engineering
  • Safety, Risk, Reliability and Quality
  • Chemical Health and Safety

Cite this

Dickeson, J. J., Miles, D., Cifdaloz, O., Wells, V., & Rodriguez, A. (2007). Robust LPV H gain-scheduled hover-to-cruise conversion for a tilt-wing rotorcraft in the presence of CG variations. In Proceedings of the IEEE Conference on Decision and Control (pp. 2773-2778). [4435028] https://doi.org/10.1109/CDC.2007.4435028

Robust LPV H gain-scheduled hover-to-cruise conversion for a tilt-wing rotorcraft in the presence of CG variations. / Dickeson, Jeffrey J.; Miles, David; Cifdaloz, Oguzhan; Wells, Valana; Rodriguez, Armando.

Proceedings of the IEEE Conference on Decision and Control. 2007. p. 2773-2778 4435028.

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

Dickeson, JJ, Miles, D, Cifdaloz, O, Wells, V & Rodriguez, A 2007, Robust LPV H gain-scheduled hover-to-cruise conversion for a tilt-wing rotorcraft in the presence of CG variations. in Proceedings of the IEEE Conference on Decision and Control., 4435028, pp. 2773-2778, 46th IEEE Conference on Decision and Control 2007, CDC, New Orleans, LA, United States, 12/12/07. https://doi.org/10.1109/CDC.2007.4435028
Dickeson JJ, Miles D, Cifdaloz O, Wells V, Rodriguez A. Robust LPV H gain-scheduled hover-to-cruise conversion for a tilt-wing rotorcraft in the presence of CG variations. In Proceedings of the IEEE Conference on Decision and Control. 2007. p. 2773-2778. 4435028 https://doi.org/10.1109/CDC.2007.4435028
Dickeson, Jeffrey J. ; Miles, David ; Cifdaloz, Oguzhan ; Wells, Valana ; Rodriguez, Armando. / Robust LPV H gain-scheduled hover-to-cruise conversion for a tilt-wing rotorcraft in the presence of CG variations. Proceedings of the IEEE Conference on Decision and Control. 2007. pp. 2773-2778
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