Skip to main navigation Skip to search Skip to main content

Adaptive control of spacecraft with uncertain flexible appendages using theory of functional connections and Integral Concurrent Learning: Numerical and testbed validation

  • Embry-Riddle Aeronautical University

Research output: Contribution to journal › Article › peer-review

Original languageEnglish
Pages (from-to)183-207
Number of pages25
JournalActa Astronautica
Volume249
DOIs
StatePublished - Dec 2026
Externally publishedYes

ASJC Scopus Subject Areas

  • Aerospace Engineering

Keywords

  • Adaptive attitude control
  • Flexible spacecraft dynamics
  • Integral concurrent learning
  • Online parameter estimation
  • Spacecraft testbed validation
  • Theory of functional connections

Cite this