NASA NTRS · 19760022207
Simulation and simulator development of a separate surface attitude command control system for light aircraft
Abstract
A 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.
Keep this discovery
Explore connections, maps & timelines
Roskam, J.. 1976-06-01. Simulation and simulator development of a separate surface attitude command control system for light aircraft. https://ntrs.nasa.gov/citations/19760022207
Cite the original work for its findings. Save a collection to share your selection of sources.