Configuration assessment and preliminary control law design for a novel diamond-shaped UAV

Stanislav Braun, Markus Geiser, Matthias Heller, Florian Holzapfel

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

16 Scopus citations

Abstract

The development of a novel aircraft configuration is typically accompanied by high technical risks. In order to ensure the success of such a development, a risk reduction phase must be considered in the design cycle.

Original languageEnglish
Title of host publication2014 International Conference on Unmanned Aircraft Systems, ICUAS 2014 - Conference Proceedings
PublisherIEEE Computer Society
Pages1009-1020
Number of pages12
ISBN (Print)9781479923762
DOIs
StatePublished - 2014
Event2014 International Conference on Unmanned Aircraft Systems, ICUAS 2014 - Orlando, FL, United States
Duration: 27 May 201430 May 2014

Publication series

Name2014 International Conference on Unmanned Aircraft Systems, ICUAS 2014 - Conference Proceedings

Conference

Conference2014 International Conference on Unmanned Aircraft Systems, ICUAS 2014
Country/TerritoryUnited States
CityOrlando, FL
Period27/05/1430/05/14

Keywords

  • Constrained Eigenstructure Assignment
  • Controllability
  • Flight Control System
  • Flight Dynamics Assessment
  • Remotely Piloted Aircraft
  • SAGITTA Demonstrator
  • Stabilization Capability
  • UAV

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