This chapter provides the basics for mathematical models used in later chapters to determine the orbital dynamics of spacecraft. The basics are coordinate systems, the physical principles stated in Kepler’s and Newton’s Laws, a discussion of work and energy, the law of conservation of total energy, angular momentum, transformations between coordinate systems, Euler angles, relative motion, and Coriolis acceleration.
Fundamentals of Astrodynamics
Orbital Mechanics and Astrodynamics ; Kapitel : 1 ; 1-22
12.01.2023
22 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Energy , Orthogonal transformation , Angular momentum , Mathematical model , Inertial frame , Astrodynamics , Euler angles , Kepler’s Laws , Conservative force , Newton’s Laws , Coriolis acceleration Physics and Astronomy , Aerospace Technology and Astronautics , Space Sciences (including Extraterrestrial Physics, Space Exploration and Astronautics) , Classical Mechanics , Engineering
TIBKAT | 2020
|Fundamentals of astrodynamics and applications
TIBKAT | 2007
|Fundamentals of Astrodynamics and Applications
AIAA | 1998
|Fundamentals of astrodynamics and applications
TIBKAT | 2001
|Review of Fundamentals of Astrodynamics and Applications
Online Contents | 1998
|