NASA NTRS · 19740023186
Multivariant function model generation
Abstract
The development of computer programs applicable to space vehicle guidance was conducted. The subjects discussed are as follows: (1) determination of optimum reentry trajectories, (2) development of equations for performance of trajectory computation, (3) vehicle control for fuel optimization, (4) development of equations for performance trajectory computations, (5) applications and solution of Hamilton-Jacobi equation, and (6) stresses in dome shaped shells with discontinuities at the apex.
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1974-01-01. Multivariant function model generation. https://ntrs.nasa.gov/citations/19740023186
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