A study of the control of micro air vehicles using the linear dynamic inverse approach

Monty J. Smith, Sean S.M. Swei, Mark B. Tischler

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

7 Scopus citations

Abstract

Results are presented from an initial investigation that considers the control of a 9-inch ducted fan driven micro air vehicle (MAV) during hover, with application of the linear dynamic inverse (DI) approach for implementation. A linear state space model based upon actual wind tunnel test data representing the hover mode is analyzed using the DI technique. The analysis shows that DI performs well with respect to stability, gain/phase margins, damping characteristics, and actuator saturation limits with 20 percent deviations in structured parameters and random model changes. A future investigation will include the performance of the MAV using the nonlinear dynamic inverse (NDI) technique for the full flight envelope, without any special consideration of a linearized operating point as done in the present analysis.

Original languageBritish English
Title of host publicationCollection of Technical Papers - AIAA 1st Intelligent Systems Technical Conference
Pages16-20
Number of pages5
StatePublished - 2004
EventCollection of Technical Papers - AIAA 1st Intelligent Systems Technical Conference - Chicago, IL, United States
Duration: 20 Sep 200423 Sep 2004

Publication series

NameCollection of Technical Papers - AIAA 1st Intelligent Systems Technical Conference
Volume1

Conference

ConferenceCollection of Technical Papers - AIAA 1st Intelligent Systems Technical Conference
Country/TerritoryUnited States
CityChicago, IL
Period20/09/0423/09/04

Fingerprint

Dive into the research topics of 'A study of the control of micro air vehicles using the linear dynamic inverse approach'. Together they form a unique fingerprint.

Cite this