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Hybrid 3-D rocket trajectory program. Part 1: Formulation and analysis. Part 2: Computer programming and user's instructionModels utilizing various sub-sets of the six degrees of freedom are used in trajectory simulation. A 3-D model with only linear degrees of freedom is especially attractive, since the coefficients for the angular degrees of freedom are the most difficult to determine and the angular equations are the most time consuming for the computer to evaluate. A computer program is developed that uses three separate subsections to predict trajectories. A launch rail subsection is used until the rocket has left its launcher. The program then switches to a special 3-D section which computes motions in two linear and one angular degrees of freedom. When the rocket trims out, the program switches to the standard, three linear degrees of freedom model.
Document ID
19740026183
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Huang, L. C. P.
(Computer Sciences Corp. Wallops Island, VA, United States)
Cook, R. A.
(Computer Sciences Corp. Wallops Island, VA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1973
Subject Category
Space Sciences
Report/Patent Number
NASA-CR-137472
Report Number: NASA-CR-137472
Accession Number
74N34296
Funding Number(s)
CONTRACT_GRANT: NAS6-2369
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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