Set theory-based spacecraft dynamics and control Chen Yang, Yuanqing Xia

Format:

Book

Author/Creator:

Yang, Chen, author.

Xia, Yuanqing, author.

Series:

Intelligent control and learning systems ; 2662-5466 v. 26

Intelligent control and learning systems 2662-5466 volume 26

Language:

English

Subjects (All):

Space vehicles--Dynamics.

Space vehicles.

Space vehicles--Control systems.

Physical Description:

1 online resource

Edition:

1st ed.

Place of Publication:

Singapore Springer [2026]

Summary:

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

Notes:

Includes bibliographical references

Online resource; title from PDF title page (SpringerLink, viewed June 2, 2026)

ISBN:

9789819591794

9819591791

OCLC:

1593564318

Access Restriction:

Restricted for use by site license