编队和集群飞行--动力学控制和设计(英文版) PDF下载 公众号 其他格式

编队和集群飞行--动力学控制和设计(英文版)

工业技术 航空、航天

  • ISBN:9787512428775
  • 作者:徐明何艳超潘晓
  • 印次:1
  • 开本:16
  • 版次:1
  • 出版社:北京航空航天大学
  • 出版时间:2019-02-01
  • 印刷时间:2019-02-01

手机扫码免费下载

纠错留言

#电子书截图

编队和集群飞行--动力学控制和设计(英文版)截图

#电子书简介

基本信息

  • 商品名称:编队和集群飞行--动力学控制和设计(英文版)
  • 作者:徐明//何艳超//潘晓
  • 定价:69
  • 出版社:北京航空航天大学
  • ISBN号:9787512428775

其他参考信息(以实物为准)

  • 出版时间:2019-02-01
  • 印刷时间:2019-02-01
  • 版次:1
  • 印次:1
  • 开本:16开
  • 包装:平装
  • 页数:266
  • 字数:343千字

内容提要

The aim of this book is to introduce the novel approaches for the study ofrelative dynamics modelling, control, and design of formation and swarm flying.Broad research focuses of current interest are covered, with each chapter involvedin different topics. The contents of this book include the introduction, definition,and property of orbital mechanics and control system in the framework offormation and swarm flying concepts using various theoretical methods andnumerical simulations, which have potential merits in mission analysis and design. The book is intended for researchers, teachers, and students of the universitiesand institutes in astrodynamics, control, and interdisciplinary space technologyfields for the purpose of academic study and engineering application.

目录

Chapter 1 Introduction
Chapter 2 Bounded Relative Orbits in the Zonal Gravitational Field
2.1 Introduction
2.2 Equations of Relative Motion Under Higher-Order Zonal Harmonic Perturbations
2.3 Bounded Relative Orbits Constraints
2.4 Bounded Relative Quasi-Periodic Orbits by the Multiple-Shooting Approach
2.5 Conclusions
Chapter 3 J2 Invariant Relative Orbits via Differential Correction Algorithm
3.1 Introduction
3.2 Hamiltonian Model for Relative Motion Dynamics
3.2.1 Coordinate Definition
3.2.2 J2 Absolute Dynamics
3.2.3 J2 Relative Dynamics
3.2.4 Perturbed Period
3.3 Existence and Denseness of Invariant Orbit
3.3.1 Existence
3.3.2 Denseness
3.4 Differential Correction
3.4.1 Correction Algorithm
3.4.2 Convergency
3.4.3 Numerical Simulation
3.5 Period and Stability of Invariant Orbit
3.5.1 Period of Invariant Orbit
3.5.2 Stable and Unstable Manifolds
3.6 Compatibility between J2 Invariant Orbit and Formation Configuration
3.6.1 Formation Configuration
3.6.2 Compatibility Definition
3.6.3 Numerical Simulation
3.7 Influences of Measure Errors on Correction
3.7.1 Dispersion Error Analysis
3.7.2 Monte Carlo Simulation
3.8 Conclusions
Chapter 4 On the Existence of J2 Invariant Relative Orbits from the Dynamical System Point of View
4.1 Introduction
4.2 J2 Hamiltonian Dynamics from Dynamical System Point of View
4.2.1 Coordinate Systems and Variables
4.2.2 Reduced Dynamics
4.2.3 PoincarE Section
4.3 Fixed Point and Its Invariant Manifolds
4.3.1 Location of the Fixed Point
4.3.2 Central Manifolds
4.4 J2 Invariant Relative Obits Generated from Fixed Points and Invariant Manifolds
4.4.1 Definition of J2 Invariant Relative Orbits
4.4.2 J2 Invariant Relative Orbits Generated from Invariant Manifolds
4.4.3 Frequency Analysis on J2 Invariant Relative Orbits
4.5 Conclusions
Chapter 5 Jn Bounded Relative Orbits Design via High-Order Poincare Maps
5.1 Introduction
5.2 Reduced Orbital Dynamics of the Zonal Problem
5.3 Differential Algebra Techniques

上一个工业技术

下一个航空、航天

  • 评论列表(0

留言评论