NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Flight dynamics analysis and simulation of heavy lift airships. Volume 1: Executive summaryA generic, yet comprehensive mathematical model and computer simulation of the HLA flight dynamics over its entire flight envelope was developed. Implicit in this simulation development are the data reviews and analyses which support the equations of motion and the calculation of forces and moments acting on the vehicle. The simulation, HYBRDS, is addressed to the broad requirements and is intended for use as a synthesis and analysis tool for the evaluation of competing HLA design concepts.
Document ID
19830013936
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ringland, R. F. (Systems Technology, Inc. Hawthorne, CA, United States)
Tischler, M. B. (Systems Technology, Inc. Hawthorne, CA, United States)
Jex, H. R. (Systems Technology, Inc. Hawthorne, CA, United States)
Emmen, R. D. (Systems Technology, Inc. Hawthorne, CA, United States)
Ashkenas, I. L. (Systems Technology, Inc. Hawthorne, CA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1982
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-166471-VOL-1
NAS 1.26:166471-VOL-1
TR-1151-2-VOL-1
Report Number: NASA-CR-166471-VOL-1
Report Number: NAS 1.26:166471-VOL-1
Report Number: TR-1151-2-VOL-1
Accession Number
83N22207
Funding Number(s)
PROJECT: RTOP 505-42-51
CONTRACT_GRANT: NAS2-10330
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available