Generalized Targeting Parameters for the Guidance of Aerospace Vehicles

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Date

1968

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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.

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Electronic Thesis or Dissertation

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