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航天器姿態(tài)動(dòng)力學(xué)中的混沌

航天器姿態(tài)動(dòng)力學(xué)中的混沌

定 價(jià):¥98.00

作 者: 劉延柱,陳立群 著
出版社: 清華大學(xué)出版社
叢編項(xiàng):
標(biāo) 簽: 工業(yè)技術(shù) 航空、航天

ISBN: 9787302282983 出版時(shí)間: 2012-10-01 包裝: 精裝
開本: 16開 頁數(shù): 163 字?jǐn)?shù):  

內(nèi)容簡(jiǎn)介

  航天器混沌姿態(tài)運(yùn)動(dòng)的識(shí)別和控制問題在航天科學(xué)中具有重要實(shí)際意義。《航天器姿態(tài)動(dòng)力學(xué)中的混沌》致力于總結(jié)該領(lǐng)域的近期發(fā)展,提供研究航天器姿態(tài)運(yùn)動(dòng)的新方法和觀點(diǎn),也為該領(lǐng)域進(jìn)一步的深入分析研究提供有明確工程背景的新的數(shù)學(xué)模型。讀者可從《航天器姿態(tài)動(dòng)力學(xué)中的混沌》獲得混沌和混沌控制理論及其在航天器姿態(tài)運(yùn)動(dòng)中應(yīng)用的知識(shí),包括基本概念,主要方法以及最新進(jìn)展。

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圖書目錄

Chapter 1 Primer on Spacecraft Dynamics
1.1 Orbital Motionof Spacecraft
1.1.1 Gravitational Field of a Particle,
1.1.2 Gravitational Field of a Rigid Body
1.1.3 Dynamical Equations of Two-body System
1.1.4 Firstlntegrals
1.1.5 Characteristics ofKeplerian Orbit
1.1.6 Elliptic Orbit
1.2 Environmental Torques Acting on Spacecraft
1.2.1 Gravitational Torque
1.2.2 Magnetic Torque
1.3 Attitude Motion of Spacecraft in the Gravitational Field
1.3.1 Euler's Equations and Poisson's Equations
1.3.2 Planar Libration
1.3.3 Stability of Relative Equilibrium
1.3.4 Attitude Motion of a Gyrostat
1.4 Attitude Motion of Torque-free Spacecraft
1.4.1 Torque-free Rigid Body,
1.4.2 Torque free Gyrostat
1.4.3 Influence of Energy Dissipation on Spinning Spacecraft
References
Chapter 2 A Survey of Chaos Theory
2.1 The Overview of Chaos
2.1.1 DescriptionsofChaos
2.1.2 Geometrical Structures of Chaos
2.1.3 Routes to Chaos
2.2 Numeri calIdentification of Chaos
2.2.1 Introduction
2.2.2 Lyapunov Exponents
2.2.3 Power Spectra
2.3 Melnikov Theory
2.3.1 Introduction
2.3.2 Transversal Homoclinic/Heteroclinic Point
2.3.3 Analytical Prediction
2.3.4 Interruptions
2.4 Chaos in Hamiltonian Systems
2.4.1 Hamiltonian Systems,lntegrability and KAM Theorem
2.4.2 Stochastic Layers and Global Chaos
2.4.3 Arnol'dDiffusion
2.4.4 Higher-Dimensional Version ofMelnikov Theory
References
Chapter 3 Chaos in Planar Attitude Motion of Spacecraft
3.1 Rigid Spacecraft in an Elliptic Orbit
3.1.1 Introduction
3.1.2 Dynamical Model
3.1.3 MelnikovAnalysis
3.1.4 Numerical Simulations
3.2 Tethered Satellite Systems
3.2.1 Introductio
3.2.2 DynamicaI Models
3.2.3 MelnikovAnalysis of the Uncoupled Case
3.2.4 Numerical Simulations
3.3 Magnetic Rigid Spacecraft in a Circular Orbit
3.3.1 Introductio
3.3.2 Dynamical Model
3.3.3 MelnikovAnalysis
3.3.4 Numericallnvestigations: Undamped Case
3.3.5 Numericallnvestigations: Damped Case
3.4 Magnetic Rigid Spacecraft in an Elliptic Orbit
3.4.1 Introductio
3.4.2 Dynamical Model
3.4.3 Melnikov Analysis
3.4.4 Numerical Simulations
References
Chapter 4 Chaos in SpatiaIAffitude Motion of Spacecraft
4.1 Attitude Motion Describedby Serret-AndoyerVariables
4.1.1 Serret-AndoyerVariables
4.1.2 Torque-free Rigid Body
4.1.3 Torque-freeGyrostat
4.1.4 Gyrostat in the Gravitational Field
4.1.5 Influence ofthe Geomagnetic Field
4.2 Rigid-body Spacecraftin an Elliptic Orbit
4.2.1 Introduction
……
Chapter 5 Control of Chaotic Attitude Motion

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