Perturbed Orbits
Perturbed Orbits
To model the effects of orbital perturbations caused by gravitational asymmetry due to oblateness and presence of a third body.
To present a simple atmospheric model for predicting the life of a satellite in a low orbit.
To introduce the concept of sphere of influence and the patched conic approach for the design and analysis of lunar and interplanetary missions.
To solve the perturbed two-body problem using numerical integration (Cowell’s and Encke’s methods).
Document information
Perturbed Orbits
Modeling,Simulation in Science(Birkhäuser)
2007-01-01
19 pages
Article/Chapter (Book)
Electronic Resource
English
Atmospheric Drag , Interplanetary Mission , Interplanetary Trajectory , Planetary Oblateness , Target Planet Engineering , Automotive Engineering , Mathematical Modeling and Industrial Mathematics , Computational Intelligence , Mathematical and Computational Engineering , Applications of Mathematics , Systems Theory, Control
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