Flight control systems capable of handling the complex operational requirements of the STOL and VTOL aircraft designs as well as designs using active control concepts are considered. Emphasis is placed on the total automatic flight control system (TACOS) (TAFCOS). Flight test results which verified the performance of the system concept are presented.
Flight tests of the total automatic flight control system (Tafcos) concept on a DHC-6 Twin Otter aircraft
1980-02-01
Report
Keine Angabe
Englisch