English (United Kingdom)

https://curated-unify.zendy.io/wp-json/zendy-region/v1/featured_content/oa?rat=en

https://curated-unify.zendy.io/wp-json/zendy-region/v1/highlighted_journal/

Zendy Open

Presents the pdf analysis as premium feature

PDF Analysis

Insights

Presents the summarisation as premium feature

Summarisation

Presents the keyphrase highlighting as premium feature

Keyphrase Highlighting

Presents the zaia usage as premium feature

ZAIA

Zendy Tools

Zendy Plus

Presents the access of premium content as premium feature

Premium Content

This paper proposes a new type of sliding mode controller termed non-switching integral sliding mode controller. It shows a certain robustness of the control system against matched uncertainty with non-switching input. Furthermore, it allows the control system to be analyzed from the aspects of the system norms, small gain theorem, and structured singular value. The validities of the proposed controller are shown by performing the numerical simulations for three different applications: a spacecraft in a displaced non-Keplerian orbit, a soft-landing problem, and a quadcopter carrying a manipulator. The potential of the proposed sliding mode control methodology is demonstrated numerically for versatility in the applications.

Design Principle of Non-Switching Integral Sliding Mode Controller and Applications to Aerospace Vehicles