The 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.
An investigation of separate surface stability augmentation systems for general aviation aircraft
1974-04-01
Report
Keine Angabe
Englisch
Utilization of Separate Surface Control Systems on General Aviation Aircraft
SAE Technical Papers | 1977
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