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Attitude determination of a high altitude balloon system. Part 1: Development of the mathematical modelA mathematical model for predicting the three dimensional motion of the balloon system is developed, which includes the effects of bounce, pendulation and spin of each subsystem. Boundary layer effects are also examined, along with the aerodynamic forces acting on the balloon. Various simplified forms of the system mathematical model were developed, based on an order of magnitude analysis.
Document ID
19750008435
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Nigro, N. J.
(Marquette Univ. Milwaukee, WI, United States)
Elkouh, A. F.
(Marquette Univ. Milwaukee, WI, United States)
Shen, K. S.
(Marquette Univ. Milwaukee, WI, United States)
Nimityongskul, P.
(Marquette Univ. Milwaukee, WI, United States)
Jhaveri, V. N.
(Marquette Univ. Milwaukee, WI, United States)
Sethi, A.
(Marquette Univ. Milwaukee, WI, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1975
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-142193
Report Number: NASA-CR-142193
Accession Number
75N16507
Funding Number(s)
CONTRACT_GRANT: NSG-1025
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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