Set Theory-Based Spacecraft Dynamics and Control (Intelligent Control and Learning Systems)

Yang, Chen/ Xia, Yuanqing

Springer Verlag, Singapore（2026/06発売）

• 製本 Hardcover:ハードカバー版／ページ数 163 p.
• 言語 ENG
• 商品コード 9789819591787

Full Description

This book presents a unified set theory-based framework for spacecraft dynamics and control under multi-source uncertainties and data-sparse conditions. First, it develops reduced-order modeling techniques for high-dimensional spacecraft dynamics by introducing interval and convex set-based uncertainty descriptions, enabling efficient model reduction while rigorously quantifying unknown-but-bounded uncertainties without reliance on large-sample statistical assumptions. Second, the book addresses spacecraft attitude determination, attitude dynamics and control problems under uncertainty, establishing interval and convex set-based formulations for attitude dynamics and different control methods, including optimal control, sliding mode control, and periodic control, and systematically integrating non-probabilistic time-dependent reliability analysis into the dynamics and control design process to simultaneously account for performance and safety requirements. Finally, the proposed methodologies are extended to rigid-flexible coupling spacecraft, where attitude motion and structural vibration interact under uncertain conditions, and set theory-based spacecraft dynamics, optimal control and bounded model predictive control strategies are developed to achieve coordinated attitude-vibration suppression with guaranteed reliability and computational efficiency. Overall, the book provides a systematic methodology that links uncertainty dynamics, control synthesis, and reliability-based design optimization, offering both solid theoretical foundations and practical tools for the dynamics and control of advanced spacecraft operating in uncertain and data-limited environments.

Contents

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.