NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Minimax attitude control of aeroballistic launch vehiclesMathematical model for determining minimax attitude control of aeroballistic launch vehicles - stability and performance of closed loop system
Document ID
19660002840
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 2, 2013
Publication Date
December 1, 1965
Subject Category
Space Sciences
Report/Patent Number
NASA-CR-350
Report Number: NASA-CR-350
Accession Number
66N12129
Funding Number(s)
CONTRACT_GRANT: NAS8-11421
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CLOSED LOOP SYSTEM
LAUNCH VEHICLE
ATTITUDE CONTROL
MATHEMATICAL MODEL
FLIGHT CONTROL
STABILITY AND CONTROL

Related Records

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