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Orbital Mechanics and Astrodynamics: Techniques and Tools for Space Missions 2015 ed. [Hardback]

  • Formāts: Hardback, 386 pages, height x width: 235x155 mm, weight: 8204 g, 10 Tables, color; 1 Tables, black and white; 9 Illustrations, color; 197 Illustrations, black and white; XVII, 386 p. 206 illus., 9 illus. in color., 1 Hardback
  • Izdošanas datums: 20-Jan-2015
  • Izdevniecība: Springer International Publishing AG
  • ISBN-10: 3319094432
  • ISBN-13: 9783319094434
Citas grāmatas par šo tēmu:
Orbital Mechanics and Astrodynamics: Techniques and Tools for Space Missions 2015 ed.Palielināt
  • Formāts: Hardback, 386 pages, height x width: 235x155 mm, weight: 8204 g, 10 Tables, color; 1 Tables, black and white; 9 Illustrations, color; 197 Illustrations, black and white; XVII, 386 p. 206 illus., 9 illus. in color., 1 Hardback
  • Izdošanas datums: 20-Jan-2015
  • Izdevniecība: Springer International Publishing AG
  • ISBN-10: 3319094432
  • ISBN-13: 9783319094434
Citas grāmatas par šo tēmu:
Permanent link: https://www.kriso.lv/db/9783319094434.html
Keywords:
This textbook covers fundamental and advanced topics in orbital mechanics and astrodynamics to expose the student to the basic dynamics of space flight. The engineers and graduate students who read this class-tested text will be able to apply their knowledge to mission design and navigation of space missions. Through highlighting basic, analytic and computer-based methods for designing interplanetary and orbital trajectories, this text provides excellent insight into astronautical techniques and tools. This book is ideal for graduate students in Astronautical or Aerospace Engineering and related fields of study, researchers in space industrial and governmental research and development facilities, as well as researchers in astronautics.This book also:· Illustrates all key concepts with examples· Includes exercises for each chapter· Explains concepts and engineering tools a student or experienced engineer can apply to mission design and navigation of space missions· Covers

fundamental principles to expose the student to the basic dynamics of space flight

Introduction.- Fundamentals of Astronautics.- Keplerian Motion.- Trajectory Correction Maneuvers.- Techniques of Astronautics.- Non-Keplerian Motion.- Spacecraft Rendezvous.- Navigation Techniques and Tools.- Further Study.- Appendix A. A Brief Review of Vector Analysis.- Appendix B: Projects.
1 Fundamentals of Astrodynamics 1(22)
1.1 Introduction
1(1)
1.2 Mathematical Models
2(3)
Use of Mathematical Models to Solve Physical Problems
2(2)
Coordinate Systems
4(1)
1.3 Physical Principles
5(8)
Kepler's Laws
5(1)
Newton's Laws
6(1)
Work and Energy
7(3)
Law of Conservation of Total Energy
10(1)
Angular Momentum
11(2)
1.4 Fundamental Transformations
13(10)
Transformations Between Coordinate Systems
13(2)
Orthogonal Transformations
15(1)
Euler Angles
16(1)
Relative Motion and Coriolis Acceleration
17(6)
2 Keplerian Motion 23(36)
2.1 Introduction
23(1)
Orbital Mechanics Versus Attitude Dynamics
23(1)
Reducing a Complex Problem to a Simplified Problem
23(1)
2.2 Two-Body Problem
24(6)
Derivation of the Equation of Motion: The Mathematical Model
24(2)
(Differential) Equation of Motion for the Two-body System
26(1)
Solution of the Equation of Motion
27(2)
An Application: Methods of Detecting Extrasolar Planets
29(1)
2.3 Central Force Motion
30(17)
Another Simplifying Assumption
30(3)
Velocity Vector
33(2)
Energy Equation
35(1)
Vis-Viva Equation
36(1)
Geometric Properties of Conic Sections
36(3)
Orbit Classification: Conic Section Orbits
39(2)
Types of Orbits
41(4)
Flight Path Angle
45(2)
2.4 Position Versus Time in an Elliptical Orbit
47(5)
Kepler's Equation
47(2)
Proving Kepler's Laws from Newton's Laws
49(3)
2.5 Astronomical Constants
52(1)
2.6 Geometric Formulas for Elliptic Orbits
52(7)
3 Orbital Maneuvers 59(68)
3.1 Introduction
59(1)
3.2 Statistical Maneuvers
59(3)
Trajectory Correction Maneuvers
59(1)
Maneuver Implementation
60(1)
Burn Models
61(1)
3.3 Determining Orbit Parameters
62(8)
Parameter Estimation
62(1)
Analytical Computations
63(1)
Graphical Presentation of Elliptical Orbit Parameters
64(5)
Circular Orbits
69(1)
Slightly Eccentric Orbits
69(1)
3.4 Orbit Transfer and Adjustment
70(11)
Single Maneuver Adjustments
71(1)
Hohmann Transfer
72(3)
Bi-elliptic Transfer
75(2)
Examples: Hohmann Transfer
77(3)
General Coplanar Transfer Between Circular Orbits
80(1)
Transfer Between Coplanar Coaxial Elliptical Orbits
80(1)
3.5 Interplanetary Trajectories
81(28)
Hyperbolic Trajectories
81(6)
Gravity Assist
87(3)
Patched Conics Trajectory Model
90(9)
Types and Examples of Interplanetary Missions
99(7)
Target Space
106(3)
Interplanetary Targeting and Orbit Insertion Maneuver Design Technique
109(1)
3.6 Other Spacecraft Maneuvers
109(6)
Orbit Insertion
109(3)
Plane Rotation
112(2)
Combined Maneuvers
114(1)
3.7 The Rocket Equation
115(12)
In Field-Free Space
115(6)
In a Gravitational Field at Launch
121(6)
4 Techniques of Astrodynamics 127(74)
4.1 Introduction
127(1)
4.2 Orbit Propagation
127(15)
Position and Velocity Formulas as Functions of True Anomaly for Any Value of e
127(1)
Deriving and Solving Barker's Equation
128(2)
Orbit Propagation for Elliptic Orbits: Solving Kepler's Equation
130(5)
Hyperbolic Form of Kepler's Equation
135(4)
Orbit Propagation for All Conic Section Orbits with e > 0: Battin's Universal Formulas
139(3)
4.3 Keplerian Orbit Elements
142(7)
Definitions
142(2)
Transformations Between Inertial and Satellite Orbit Reference Frames
144(1)
Conversion from Inertial Position and Velocity Vectors to Keplerian Orbital Elements
145(2)
Conversion from Keplerian Elements to Inertial Position and Velocity Vectors in Cartesian Coordinates
147(1)
Alternative Orbit Element Sets
148(1)
4.4 Lambert's Problem
149(21)
Problem Statement
149(1)
A Mission Design Application
150(4)
Trajectories/Flight Times Between Two Specified Points
154(11)
Mission Design Application (Continued)
165(1)
Parametric Solution Tool and Technique
166(4)
A Fundamental Problem in Astrodynamics
170(1)
4.5 Celestial Mechanics
170(21)
Legendre Polynomials
171(2)
Gravitational Potential for a Distributed Mass
173(10)
The n-Body Problem
183(2)
Disturbed Relative 2-Body Motion
185(3)
Sphere of Influence
188(3)
4.6 Time Measures and Their Relationships
191(10)
Introduction
191(1)
Universal Time
192(1)
Atomic Time
193(1)
Dynamical Time
193(1)
Sidereal Time
194(1)
Julian Days
194(1)
What Time Is It in Space?
194(7)
5 Non-Keplerian Motion 201(22)
5.1 Introduction
201(1)
5.2 Perturbation Techniques
201(5)
Perturbations
202(2)
Special Perturbations
204(1)
Osculating Ellipse
205(1)
5.3 Variation of Parameters Technique
206(2)
In-Plane Perturbation Components
206(1)
Out-of-Plane (or Lateral) Perturbation Component
207(1)
Summary
208(1)
5.4 Oblateness Effects: Precession
208(6)
Potential Function for an Oblate Body
208(1)
Oblateness
209(2)
Precession of the Line of Nodes
211(3)
5.5 An Alternate Form of the Perturbation Equations
214(1)
RTW (Radial, Transverse, and Out-of-Plane) Coordinate System
214(1)
Perturbation Equations of Celestial Mechanics
215(1)
5.6 Primary Perturbations for Earth-Orbiting Spacecraft
215(1)
5.7 Satellite Orbit Paradox
215(6)
Introduction
215(1)
Keplerian Orbit
216(1)
Orbit Paradox
216(2)
Applications
218(3)
5.8 "Zero G"
221(2)
6 Spacecraft Rendezvous 223(20)
6.1 Introduction
223(1)
6.2 Phasing for Rendezvous
224(1)
Alternative Transfer Orbits
225(1)
6.3 Example: Apollo 11 Ascent from the Moon
225(1)
6.4 Terminal Rendezvous
226(11)
Equations of Relative Motion for a Circular Target Orbit
226(4)
Hill's Equations
230(1)
Solutions for the Hill—Clohessy—Wiltshire Equations
231(2)
Example: Standoff Position to Avoid Collision with the Target Vehicle
233(1)
Spacecraft Intercept or Rendezvous with a Target Vehicle
233(4)
6.5 Examples of Spacecraft Rendezvous
237(1)
Space Shuttle Discovery's Rendezvous with the ISS
237(1)
Mars Sample Return
238(1)
6.6 General Results for Terminal Spacecraft Rendezvous
238(5)
Particular Solutions (f not = to 0)
238(1)
Target Orbits with Non-Zero Eccentricity
238(1)
Highly Accurate Terminal Rendezvous
239(1)
General Algorithm
239(4)
7 Navigation and Mission Design Techniques and Tools 243(82)
7.1 Introduction
243(1)
7.2 Online Ephemeris Websites
243(4)
Solar System Dynamics Website: ssd
244(2)
Near Earth Objects Website: neo
246(1)
Potentially Hazardous Asteroids
247(1)
7.3 Maneuver Design Tool
247(9)
Flight Plane Velocity Space (FPVS)
247(5)
Maneuver Design Examples
252(2)
Maneuver Considerations
254(1)
Algorithm for Computing Gradients in FPVS
254(2)
7.4 Free-Return Circumlunar Trajectory Analysis Techniques
256(69)
Introduction
256(1)
Apollo Program
257(1)
Free-Return Circumlunar Trajectory Analysis Method 1
258(10)
Free-Return Circumlunar Trajectory Analysis Method 2
268(57)
8 Further Study 325(12)
8.1 Introduction
325(1)
8.2 Additional Navigation, Mission Analysis and Design, and Related Topics
325(12)
Mission Analysis and Design
325(1)
Orbit Determination
326(1)
Launch
327(1)
Spacecraft Attitude Dynamics
327(1)
Spacecraft Attitude Determination and Control
328(1)
Constellations
328(1)
Earth-Orbiting Constellations
329(1)
Mars Network
329(1)
Formation Flying
329(1)
Aerogravity Assist (AGA)
330(1)
Lagrange Points and the Interplanetary Superhighway
331(1)
Solar Sailing
331(1)
Entry, Decent and Landing (EDL)
332(1)
Cyclers
332(1)
Spacecraft Propulsion
333(1)
Advanced Spacecraft Propulsion
334(3)
Appendix A Vector Analysis 337(12)
Appendix B Projects 349(8)
Appendix C Additional Penzo Parametric Plots 357(8)
Answers to Selected Exercises 365(4)
Acronyms and Abbreviations 369(4)
References 373(6)
Index 379
Prof. Gerald Hintz is an Adjunct Professor in the Astronautical Engineering Department at the University of Southern California. He is also a Senior Engineer and Functional Area Manager for the Spacecraft Navigation at the Jet Propulsion Laboratory.