Generalized Targeting Parameters for the Guidance of Aerospace Vehicles
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Date
1968
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Publisher
University of Alabama Libraries
Abstract
This thesis presents the development of the equations necessary to compute the targeting parameters for the iterative guidance mode for all types of space missions. A brief introduction to the iterative guidance mode is presented as well as the derivation and explanation of the necessary equations to compute the targeting parameters. Experimental verification of the equations is also included.
Description
Electronic Thesis or Dissertation