Robust Flight Control Using Incremental Nonlinear Dynamic Inversion and Angular Acceleration Prediction

S Sieberling, QP Chu, JA Mulder

Research output: Contribution to journalArticleScientificpeer-review

331 Citations (Scopus)
Original languageEnglish
Pages (from-to)1732-1742
Number of pages11
JournalJournal of Guidance, Control, and Dynamics: devoted to the technology of dynamics and control
Volume33
Issue number6
Publication statusPublished - 2010

Keywords

  • CWTS JFIS < 0.75

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