
Orbital Mechanics for Engineering Students
Revised Reprint
by Howard D. Curtis
4th Edition
Publisher: Elsevier Butterworth Heinemann
Book Details
| Print ISBN | 9780128240250 |
| eText ISBN | 9780323853453 |
| Publisher | Elsevier Butterworth Heinemann |
| Publishing Year | 2021 |
| Edition | 4th Edition |
| Language | English |
| Pages | 780 |
Aspiring aerospace engineers require a rigorous yet highly accessible foundation to navigate the complexities of modern space mission design. **Orbital Mechanics for Engineering Students 4th Edition** delivers exactly this, serving as an indispensable academic resource in an era of rapidly expanding commercial spaceflight and deep-space exploration. Howard D. Curtis provides a masterfully structured introduction to the mathematical and physical principles governing spacecraft motion. By balancing theoretical depth with practical engineering applications, this updated volume ensures that students and practicing aerospace professionals can confidently analyze orbital trajectories, plan complex maneuvers, and understand the dynamics of satellite attitude control in a rapidly evolving global aerospace landscape.
The textbook's comprehensive scope spans the fundamental physics of point masses to the intricate dynamics of rigid bodies and multi-stage rocket vehicles. Curtis employs a highly effective, practical teach-by-example methodology, guiding readers through the classical two-body problem, three-dimensional orbits, and preliminary orbit determination. Key themes include coordinate transformations, orbital perturbations, and relative motion, which are critical for rendezvous operations. The author's analytical perspective is bolstered by robust computational tools, particularly downloadable MATLAB algorithms, which empower students to translate abstract mathematical formulations into functional, real-world engineering simulations. This seamless blend of theory and computation provides a holistic view of modern astrodynamics.
Designed primarily for upper-level undergraduate and introductory graduate courses in aerospace engineering, **Orbital Mechanics for Engineering Students 4th Edition** stands out for its exceptional pedagogical support and student-focused design. This revised edition introduces a brand-new chapter on the circular restricted three-body problem, including low-energy trajectories, alongside updated coverage of interplanetary mission design, lunar missions, and non-Hohmann transfers. Instructors and students benefit from an extensive support package containing fully worked solutions, PowerPoint lecture slides, and interactive animations of selected topics. For those seeking a flexible digital learning experience, the **Orbital Mechanics for Engineering Students 4th Edition PDF** offers seamless, anytime access to these vital resources, making it the premier choice for academic institutions worldwide.
Table of Contents
Chapter 1: Dynamics of point masses
- • Kinematics
- • Mass, force and Newton's law of gravitation
- • Newton's law of motion
- • Time derivatives of moving vectors
- • Relative motion
Chapter 2: The two-body problem
- • Equations of motion in an inertial frame
- • Equations of relative motion
- • Angular momentum and the orbit formulas
- • The energy law
- • Circular, elliptical, parabolic, and hyperbolic orbits
- • Perifocal frame
- • The Lagrange coefficients
- • Restricted three-body problem
Chapter 3: Orbital position as a function of time
- • Time since periapsis
- • Kepler's equation for elliptical, parabolic, and hyperbolic orbits
- • Universal variables
Chapter 4: Orbits in three dimensions
- • Geocentric right ascension-declination frame
- • State vector and the geocentric equatorial frame
- • Orbital elements and the state vector
- • Coordinate transformations
- • Effects of the earth's oblateness
Chapter 5: Preliminary orbit determination
- • Gibbs' method
- • Lambert's problem
- • Sidereal time
- • Topocentric coordinate systems
- • Gauss's method
Chapter 6: Orbital maneuvers
- • Impulsive maneuvers
- • Hohmann and bi-elliptic transfers
- • Phasing maneuvers
- • Non-Hohmann transfers
- • Apse line rotation
- • Plane change maneuvers
Chapter 7: Relative motion and rendezvous
- • Relative motion in orbit
- • Clohessy-Wiltshire equations
- • Two-impulse rendezvous maneuvers
Chapter 8: Interplanetary trajectories
- • Interplanetary Hohmann transfers
- • Rendezvous opportunities
- • Sphere of influence
- • Method of patched conics
- • Planetary departure, flyby, and arrival
Chapter 9: Lunar trajectories
- • Motion in the Earth-Moon system
- • Lunar flight trajectory design
- • Patched conic approximation for lunar missions
Chapter 10: Introduction to orbital perturbations
- • Non-spherical Earth gravity
- • Atmospheric drag
- • Solar radiation pressure
- • Third-body gravity perturbations
Chapter 11: Rigid body dynamics
- • Kinematics of rigid bodies
- • Equations of translational and rotational motion
- • Moments of inertia
- • Euler's equations
- • Euler angles
Chapter 12: Spacecraft attitude dynamics
- • Torque-free motion and stability
- • Dual-spin spacecraft
- • Nutation dampers
- • Attitude control thrusters
- • Yo-yo despin mechanism
- • Gyroscopic attitude control
- • Gravity-gradient stabilization
Chapter 13: Rocket vehicle dynamics
- • Equations of motion and the thrust equation
- • Rocket performance
- • Restricted and optimal staging
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