Special functions of an advanced control system were investigated for effects on spin entries and recoveries utilizing a 3/8-scale model of the F-15 airplane as a remotely piloted research vehicle (RPRV). Telemetry uplinks and downlinks were used with a ground-based digital computer to mechanize the RPRV control system for spin tests in flight. Results from the model RPRV flight tests and from a real time digital spin simulation were used to evaluate the F-15 stall inhibiter and an automatic spin recovery system developed for the RPRV model
Remotely piloted research vehicle evaluation of advanced control system effects on spins
Atmospheric Flight Mechanics Conference ; 1976 ; Arlington, TX
1976-01-01
Miscellaneous
No indication
English
NTIS | 1978
|NTIS | 1978
|Remotely Piloted Vehicle Technology
SAE Technical Papers | 1972
|