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
No indication
English
SAE Technical Papers | 1981
|Pilot Workload Assessment for NO AFCS Mission Helicopter Dispatch
British Library Conference Proceedings | 2011
|