Orbital Mechanics for Engineering Students, Second Edition, provides an introduction to the basic concepts of space mechanics. These include vector kinematics in three dimensions; Newton’s laws of motion and gravitation; relative motion; the vector-based solution of the classical two-body problem; derivation of Kepler’s equations; orbits in three dimensions; preliminary orbit determination; and orbital maneuvers. The book also covers relative motion and the two-impulse rendezvous problem; interplanetary mission design using patched conics; rigid-body dynamics used to characterize the attitude of a space vehicle; satellite attitude dynamics; and the characteristics and design of multi-stage launch vehicles. Each chapter begins with an outline of key concepts and concludes with problems that are based on the material covered. This text is written for undergraduates who are studying orbital mechanics for the first time and have completed courses in physics, dynamics, and mathematics, including differential equations and applied linear algebra. Graduate students, researchers, and experienced practitioners will also find useful review materials in the book. NEW: Reorganized and improved discusions of coordinate systems, new discussion on perturbations and quarternions NEW: Increased coverage of attitude dynamics, including new Matlab algorithms and examples in chapter 10 New examples and homework problems
An obvious alternative to the coning maneuver is to use thrusters RCS-3 and 4 to despin the craft completely, thrusters RCS-5 and 6 to initiate roll around the y axis and stop it after 90◦, and then RCS-3 and 4 to respin the spacecraft ...
The superb examples will be extremely valuable to undergraduates and distinguishes this text from many others. This book should be given serious consideration for any undergraduate course in orbital mechanics or spacecraft dynamics.
B.2 Online Ephemeris Project for an Asteroid Background for Asteroids Events for asteroids are: 1. Discovery 2. ... 1/24/08) Some facts about asteroids are: The first asteroid, 1 Ceres, was discovered by Giuseppe Piazzi in January 1801.
Teaching text developed by U.S. Air Force Academy and designed as a first course emphasizes the universal variable formulation.
A lively study of orbital mechanics by the writer responsible for the computer simulations and systems analysis for the Saturn V moon rocket, Project Skylab and many others.
Completely revised and updated, this edition provides: * Current data and statistics, along with coverage of new research and the most recent developments in the field * Three new chapters: "The Three-Body Problem" (Ch. 4), "Continuous ...
... DC (1966) Deprit, A., Pickard, H., Poplarchek, W.: Compression of ephemerides by discrete Chebyshev approximations. ... K.T.: Precise ephemeris reconstruction using the Clohessy-Wiltshire frame and multiple sequential compressions.
Comprehensive, classic introduction to space-flight engineering for advanced undergraduate and graduate students provides basic tools for quantitative analysis of the motions of satellites and other vehicles in space.
The book is filled with illustrated concepts and real-world examples drawn from the space industry. Additionally, the book includes a “computational toolbox” composed of MATLAB M-files for performing space mission analysis.
Analytical Mechanics of Space Systems