طراحی مأموریت فضاپیما، ویرایش دوم (سری آموزش AIAA)

The 2nd edition of "Spacecraft Mission Design" takes a short route to practical understanding of mission design. It focuses on the most general and most practical tools needed for the early spacecraft design studies, including the principles of two-body motion, definition of orbits, orbital manoeuvres and central body observation. The use of elementary mathematics makes this concise book ideal for college upperclassmen, graduates and practising engineers or managers. There are enough worked examples that one can be self-taught. This 2nd edition includes astronomical reference material, sections on constellations, lunar trajectories, and cycler orbits. In addition, the ORBWIN AIAA Mission Design software has been totally rewritten to make it easier to use and compatible with Windows. ORBWIN allows you to proceed directly from understanding into professional work. It provides the accuracy, speed and convenience of personal computing. It defines orbital elements for any orbit, provides the parameters at any orbital point, calculates spacecraft horizon, instrument field of view, orbit perturbations, ground track, planetary ephemeris, conversion of Julian days, oblique triangle solutions, and propellant weight projections. Cover Title Copyright Table of Contents Preface Chapter 1. Introduction 1.1 Arrangement of the Book 1.2 ORBWIN: AIAA Mission Design Software 1.3 Study of Two-Body Motion Chapter 2. Two-Body Motion 2.1 Circular Orbits 2.2 General Solution 2.3 Elliptical Orbits 2.4 Parabolic Orbits 2.5 Hyperbolic Orbits 2.6 Time Systems 2.7 Coordinate Systems 2.8 Classical Orbital Elements Problems Chapter 3. Orbital Maneuvers 3.1 In-Plane Orbit Changes 3.2 Hohmann Transfer 3.3 Bielliptical Transfer 3.4 Plane Changes 3.5 Combined Maneuvers 3.6 Propulsion for Maneuvers Problems Chapter 4. Observing the Central Body 4.1 Effect of the Launch Site 4.2 Orbit Perturbations 4.3 Ground Track 4.4 Spacecraft Horizon 4.5 Constellations Problems Chapter 5. Special Earth Orbits 5.1 Geosynchronous Orbit 5.2 Sun-Synchronous Orbit 5.3 Molniya Orbit 5.4 Low Earth Orbit Problems Chapter 6. Interplanetary Trajectories 6.1 Patched Conic Approximation 6.2 Highly Simplified Example 6.3 Patched Conic Procedure 6.4 Locating the Planets 6.5 Design of the Transfer Ellipse 6.6 Design of the Departure Trajectory 6.7 Design of the Arrival Trajectory 6.8 Gravity-Assist Maneuver 6.9 Cycler Orbits 6.10 Establishing Planetary Orbit Problems Chapter 7. Lunar Trajectories 7.1 Motion of the Earth-Moon System 7.2 Time of Flight and Injection Velocity 7.3 Sphere of Influence 7.4 Lunar Patched Conic Problems Appendix A. ORBWIN: AIAA Mission Design Software A.1 Introduction to ORBWIN A.2 Quick Tour of ORBWIN A.3 Orbit Definition Example A.4 Utilities A.5 Interesting Orbits—Examples Appendix B. Mission Design Glossary Appendix C. Mission Design Data References Index

Spacecraft Mission Design, Second Edition, takes the shortest route to practical understanding of mission design. It focuses on the most general and most practical tools needed for the early spacecraft design studies, including the principles of two-body motion, definition of orbits, orbital maneuvers, and central body observation. The use of elementary mathematics makes this concise book ideal for upper class college students, graduates, and practicing engineers or managers. There are enough worked examples that one can be self-taught.

This second edition includes astronomical reference material and sections on constellations, lunar trajectories, and cycler orbits. The software ORBWIN allows you to proceed directly from understanding into professional work. It provides the accuracy, speed, and convenience of personal computing. It defines all orbital elements for any orbit, provides the parameters at any orbital point, calculates spacecraft horizon, instrument field of view, orbit perturbations, ground track, planetary ephemeris, conversion of Julian days, oblique triangle solutions, and propellant weight projections. Any major body in the solar system may be used as the central body.

System Requirements: Windows 3.11 or higher, 8 Mb RAM, 3.5-inch disk drive.

This text focuses on the most general and most practical tools needed for the early spacecraft design studies, including the principles of two-body motion, definition of orbits, orbital maneuvers, and central body observation. The use of elementary mathematics makes this concise book ideal for upperclass college students, graduates, and practicing engineers or managers. There are enough worked examples that one can be self taught. The second edition includes astronomical reference material, sections on constellations, lunar trajectories, and cycler orbits. ORBWIN allows you to proceed directly from understanding into professional work. It defines all orbital elements for any orbit, provides the parameters at any orbital point, calculates spacecraft horizon, instrument field of view, orbit perturbations, ground track, planetary ephemeris, conversion of Julian days, oblique triangle solutions, and propellant weight projections. Any major body in the solar system may be used as the central body. This book and accompanying software offer the reader a practical understanding of mission design. The text focuses on the most general and practical tools needed for the early spacecraft design studies (principles of two-body motion, definition of orbits, central body observation).