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. In-flight model parameter and state estimation using gradient descent for high-speed flight

    Research output: Contribution to journalArticleScientificpeer-review

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Activities

  1. Springer (Publisher)

    Activity: Publication peer-review and editorial workEditorial activity

  2. AVIC-TU Delft Advanced Technology Seminar

    Activity: Talk or presentationTalk or presentation at a workshop, seminar, course or other meeting

  3. The use of Adaptive Nonlinear Dynamic Inversion for Fault Tolerant Flight Control, application to civil aircraft

    Activity: Talk or presentationTalk or presentation at a workshop, seminar, course or other meeting

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ID: 96391