An acceleration measurements-based approach for helicopter nonlinear flight control using Incremental Nonlinear Dynamic Inversion

Research output: Contribution to journalArticleScientificpeer-review

98 Citations (Scopus)
Original languageEnglish
Pages (from-to)1065-1077
Number of pages13
JournalControl Engineering Practice
Volume21
Issue number8
Publication statusPublished - 2013

Keywords

  • CWTS 0.75 <= JFIS < 2.00

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