Dynamic modeling of large-scale morphing aircraft

Thomas M. Seigler, David A. Neal, Daniel J. Inman

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

17 Scopus citations

Abstract

The dynamics of morphing flight, in which large changes in structural geometry may occur, include various components that are not apparent in the standard rigid flight equations. The additional terms include parameter and/or time varying aerodynamic forces and inertial forces due to relative motion. Here we study the importance of the inertial forces and moments, in particular those involving rate terms, with the goal of reducing the dynamics that must be considered in a flight control design. The dynamics are analyzed within the framework of the standard longitudinal flight assumptions and an example is given, constructed to be typical of a modern large-scale morphing aircraft.

Original languageEnglish
Title of host publicationCollection of Technical Papers - 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Subtitle of host publication14th AIAA/ASME/AHS Adaptive Structures Conference, 8th AIAA Non-deterministic App
Pages3668-3678
Number of pages11
DOIs
StatePublished - 2006
Event47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference - Newport, RI, United States
Duration: May 1 2006May 4 2006

Publication series

NameCollection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Volume5
ISSN (Print)0273-4508

Conference

Conference47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Country/TerritoryUnited States
CityNewport, RI
Period5/1/065/4/06

ASJC Scopus subject areas

  • Architecture
  • General Materials Science
  • Aerospace Engineering
  • Mechanics of Materials
  • Mechanical Engineering

Fingerprint

Dive into the research topics of 'Dynamic modeling of large-scale morphing aircraft'. Together they form a unique fingerprint.

Cite this