Adaptive Linear Parameter Varying Control for Aeroservoelastic Suppression

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX11CD58P
Agency Tracking Number: 105480
Amount: $99,994.00
Phase: Phase I
Program: SBIR
Awards Year: 2011
Solicitation Year: 2010
Solicitation Topic Code: A1.07
Solicitation Number: N/A
Small Business Information
MN, Minneapolis, MN, 55414-5377
DUNS: 781726104
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Peter Seiler
 Principal Investigator
 (734) 262-0820
 peter.j.seiler@gmail.com
Business Contact
 Gary Balas
Title: Business Official
Phone: (651) 602-9732
Email: balas@musyn.com
Research Institution
 Stub
Abstract
Adaptive control offers an opportunity to fulfill present and futureaircraft safety objectives though automatedvehicle recovery while maintaining performanceand stability requirements in the presence of unknown orvarying operating environment.Future aircraft are a natural application of adaptive control. Theseaircraft will be more fuel efficient, have longer operating ranges thoughmore flexible aircraft structures. Thisincreased flexibility will result in structural modes being in thesame frequency range as the rigid body modes. The traditionalnon-adaptive control design approach to address the aeroservoelastic (ASE)interaction of decoupling the rigid body and structural dynamicswill not work. Furthermore, the application of adaptive controlto these flexible aircraft may result inundesired ASE excitationleading to structural damage or failure. Hencean integrated flight control system is needed for gust loadalleviation, flutter suppression and rigid body control of theaircraft which works in concert with the adaptive control systemfor improved resilience and safety.MUSYN proposes an integrated approach based on linear, parameter-varying(LPV) control to the design of theflight control, load alleviation and flutter suppression algorithms.The Phase I and Phase II research will focus on applying andextending LPV techniques to model, design, analyze andsimulate control algorithms for flexible aircraft.The objective is to combine the integratedLPV flight control system with adaptive control topreserve rigid body performance during upsets while retaining the loadalleviation and flutter suppression characteristics of thenominally augmented aircraft.Phase I will develop a prototype LPV framework for modeling, analysis,control and simulation and Phase II will develop a comprehensiveLPV software tool suite.

* Information listed above is at the time of submission. *

Agency Micro-sites

SBA logo
Department of Agriculture logo
Department of Commerce logo
Department of Defense logo
Department of Education logo
Department of Energy logo
Department of Health and Human Services logo
Department of Homeland Security logo
Department of Transportation logo
Environmental Protection Agency logo
National Aeronautics and Space Administration logo
National Science Foundation logo
US Flag An Official Website of the United States Government