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Simulation and simulator development of a separate surface attitude command control system for light aircraftA detailed description is presented of the simulation philosophy and process used in the development of a Separate Surface Attitude Command control system (SSAC) for a Beech Model 99 Airliner. The intent of this system is to provide complete three axes stability augmentation at low cost and without the need for system redundancy. The system, although aimed at the general aviation market, also has applications to certain military airplanes as well as to miniature submarines.
Document ID
19760022207
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Roskam, J.
(Kansas Univ. Lawrence, KS, United States)
Date Acquired
August 8, 2013
Publication Date
June 1, 1976
Publication Information
Publication: AGARD Flight Simulation(Guidance Systems Simulation
Subject Category
Aircraft Stability And Control
Accession Number
76N29295
Distribution Limits
Public
Copyright
Other
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