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Computational Methods for Nonlinear Dynamical Systems - Theory and Applications in Aerospace Engineering (Paperback): Xuechuan... Computational Methods for Nonlinear Dynamical Systems - Theory and Applications in Aerospace Engineering (Paperback)
Xuechuan Wang, Xiaokui Yue, Honghua Dai, Haoyang Feng, Satya N Atluri
R3,835 R3,390 Discovery Miles 33 900 Save R445 (12%) Ships in 12 - 17 working days

Computational Methods for Nonlinear Dynamical Systems: Theory and Applications in Aerospace Engineering proposes novel ideas and develops highly-efficient and accurate methods for solving nonlinear dynamic systems, drawing inspiration from the weighted residual method and the asymptotic method. Proposed methods can be used both for real-time simulation and the analysis of nonlinear dynamics in aerospace engineering. The book introduces global estimation methods and local computational methods for nonlinear dynamic systems. Starting from the classic asymptotic, finite difference and weighted residual methods, typical methods for solving nonlinear dynamic systems are considered. In addition, new high-performance methods are proposed, such as time-domain collocation and local variational iteration. The book summarizes and develops computational methods for strongly nonlinear dynamic systems and considers the practical application of the methods within aerospace engineering.

Spacecraft Attitude Control - A Linear Matrix Inequality Approach (Paperback): Chuang Liu, Xiaokui Yue, Keke Shi, Zhaowei Sun Spacecraft Attitude Control - A Linear Matrix Inequality Approach (Paperback)
Chuang Liu, Xiaokui Yue, Keke Shi, Zhaowei Sun
R3,403 Discovery Miles 34 030 Ships in 12 - 17 working days

Spacecraft Attitude Control: A Linear Matrix Inequality Approach solves problems for spacecraft attitude control systems using convex optimization and, specifi cally, through a linear matrix inequality (LMI) approach. High-precision pointing and improved robustness in the face of external disturbances and other uncertainties are requirements for the current generation of spacecraft. This book presents an LMI approach to spacecraft attitude control and shows that all uncertainties in the maneuvering process can be solved numerically. It explains how a model-like state space can be developed through a mathematical presentation of attitude control systems, allowing the controller in question to be applied universally. The authors describe a wide variety of novel and robust controllers, applicable both to spacecraft attitude control and easily extendable to second-order systems. Spacecraft Attitude Control provides its readers with an accessible introduction to spacecraft attitude control and robust systems, giving an extensive survey of current research and helping researchers improve robust control performance.

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