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Multivariant function model generationThe 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.
Document ID
19740023186
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
January 1, 1974
Subject Category
Space Sciences
Report/Patent Number
NASA-CR-139443
Accession Number
74N31299
Funding Number(s)
CONTRACT_GRANT: NGR-01-003-008
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19740023187WorkA method for determining optimum re-entry trajectories19740023188WorkResearch on development of equations for performance trajectory computations19740023189WorkVehicle control for fuel optimization19740023190WorkResearch on development of equations for performance trajectory computation19740023191WorkSome suggested approaches to solving the Hamilton-Jacobi equation associated with constrained rigid body motion19740023192WorkHamilton/Jacobi perturbation methods applied to the rotational motion of a rigid body in a gravitational field19740023193WorkStresses in dome-shaped shells of revolution with discontinuities at the apex
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