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A compilation of 33 papers presented at the 10th anniversary meeting of the Upper Atmosphere Rocket Research Panel, Jan. 26-27, 1956, University of Michigan, Ann Arbor. Cf. Pref. to 1st ed.
Analytical solutions to the orbital motion of celestial objects have been nowadays mostly replaced by numerical solutions, but they are still irreplaceable whenever speed is to be preferred to accuracy, or to simplify a dynamical model. In this book, the most common orbital perturbations problems are discussed according to the Lie transforms method, which is the de facto standard in analytical orbital motion calculations.
The geodetic use of rockets, artificial satellites, and the moon is reviewed. The discussion covers in turn dynamics, geometry, observational techniques, comparison with terrestrial geodesy, and geophysical implications. (AUHOR).