Product Description
Orbital and Celestial Mechanics affords engineering students, professors, and researchers alike an opportunity to cultivate the mathematical techniques necessary for this discipline-as well as physics and trajectory mechanics-using the familiar and universal concepts of classical physics. For nonspecialists and students unfamiliar with some of the underlying mathprinciples, the Vinti Spheroidal Method demonstrates computer routines for accurately calculating satellite orbit and ballistic trajectory. More than 20 years ago, Dr. Vinti's revolutionary method was used aboard a ballistic missile targeting program with great success. His work continues to enable both students and professionals to predict position and velocity vectorsfor satellites and ballistic missiles almost as accurately as numerical integration. Now, the best Vinti algorithms and companion computer source codes are available.
System Requirements: Software is compatible to PCs with Windows 95 and MicroSoft FORTRAN and Visual C++ Powerstation 4.0; also mentions UNIX Powerstation with Vi editor.
About the Author
Dr. Vinti received both his B.S. degree in mathematics (1927) and D.Sc. degree in physics (1932) from MIT. While researching at the Aberdeen Proving Ground in Maryland, he joined the National Bureau of Standards in 1957. One of his most noteworthy papers, "The Calculation of the Continuous Absorption Spectrum of Helium," is referenced in the Encyclopedia of Physics.
