DOI

The paper is devoted to design and experimental testing the adaptive identification algorithms of pitch and elevation model parameters for "LAAS Helicopter Benchmark". The adaptive identification algorithms for separate pitch and elevation motions are proposed and the experimental results are presented. Laboratory experiments clarify the properties of the adaptive identification algorithms in real-world conditions.

Original languageEnglish
Title of host publication16th IEEE International Conference on Control Applications, CCA 2007. Part of IEEE Multi-conference on Systems and Control
Pages825-830
Number of pages6
DOIs
StatePublished - 2007
Event16th IEEE International Conference on Control Applications, CCA 2007. Part of IEEE Multi-conference on Systems and Control - , Singapore
Duration: 1 Oct 20073 Oct 2007

Publication series

NameProceedings of the IEEE International Conference on Control Applications

Conference

Conference16th IEEE International Conference on Control Applications, CCA 2007. Part of IEEE Multi-conference on Systems and Control
Country/TerritorySingapore
Period1/10/073/10/07

    Scopus subject areas

  • Engineering(all)

ID: 87382485