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An investigation of separate surface stability augmentation systems for general aviation aircraftThe status of a project to develop and evaluate separate surface stability augmentation systems for general aviation aircraft is discussed. The electrical design, roll heading hold is described and schematic diagrams and an operational description are provided. The flight tests program is explained. Various failure conditions are proposed and the effects on the stability of the aircraft are analyzed.
Document ID
19740013534
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
April 1, 1974
Subject Category
Aircraft
Report/Patent Number
NASA-CR-138120
PR-9
Report Number: NASA-CR-138120
Report Number: PR-9
Accession Number
74N21647
Funding Number(s)
CONTRACT_GRANT: NGR-17-002-095
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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