
Teil der Reihe: Mathematics and Statistics (R0)
Set Theory-Based Spacecraft Dynamics and Control
Inhaltsangabe
Introduction.- Interval-oriented Reduced-order Model for Uncertain Systems.- Convex Model-based Reduced-order Model for Uncertain Control Systems.- Uncertain robust attitude determination based on set theory.- Uncertain optimal attitude control for space power satellite based on interval Riccati equation with non-probabilistic time-dependent reliability.- Uncertain iterative optimal attitude control method for periodic satellite with reliability constraint.- Reliability-constrained uncertain spacecraft sliding mode attitude control with set theory.- Reliability-constrained optimal attitude-vibration control for rigid-flexible coupling satellite using interval dimension-wise analysis.- Bounded model predictive control for rigid-flexible coupling satellite with reliability constraint.- Hybrid-uncertainty-based attitude control for rigid-flexible satellite considering degradation and non-probabilistic reliability.
Produktdetails
- Erscheinungsdatum: 16.05.2026
- Autor/Autorin: Chen Yang,Yuanqing Xia
- Reihe: Mathematics and Statistics (R0)
- Format: E-Book
- Dateiformat: PDF
- Kopierschutz: Wasserzeichen
- Dateigröße: 15.6 MB
- Verlag: SPRINGER
- Sprache: Englisch
- Umfang: 206 Seiten
- ISBN: 9789819591794
- Lieferung: Sofort per Download
- Hinweis: Sofort per Download lieferbar. Kein physischer Versand.
- Kompatibilität: Lesbar auf Geräten und Apps mit PDF-Unterstützung.
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