Research output

  1. Flexible Aircraft Gust Load Alleviation with Incremental Nonlinear Dynamic Inversion

    Research output: Contribution to journalArticleScientificpeer-review

  2. Comparison of three control structures for inducing higher-order sliding modes

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

  3. Incremental Backstepping Sliding Mode Fault-Tolerant Flight Control

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

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ID: 166351