A mathematical model for the autostabilizer/autopilot mode of the automatic flight control system (AFCS) for the Sea King Mk.50 helicopter is presented. An outline of the autostabilizer/autopilot used in the aircraft is given first, followed by a description of the mathematical model, which includes a representation of each major element of the aircraft system. (Author)
Sea King Mk. 50 Helicopter Flight Control System. A Mathematical Model of the AFCS (Autostabilizer/Autopilot Mode)
1979
28 pages
Report
Keine Angabe
Englisch
SAE | 1981
|A-7A AFCS -- Flight-proved high-gain system
Engineering Index Backfile | 1966
|