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NASA NTRS ยท 19720021013

G and C boost and abort study summary, exhibit B

Abstract

A six degree of freedom simulation of rigid vehicles was developed to study space shuttle vehicle boost-abort guidance and control techniques. The simulation was described in detail as an all digital program and as a hybrid program. Only the digital simulation was implemented. The equations verified in the digital simulation were adapted for use in the hybrid simulation. Study results were obtained from four abort cases using the digital program.

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BibTeXRIS

Backman, H. D.. 1972-06-30. G and C boost and abort study summary, exhibit B. https://ntrs.nasa.gov/citations/19720021013

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