Remotely piloted research vehicle evaluation of advanced control system effects on spinsSpecial 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
Document ID
19760053941
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Petersen, K. L. (NASA Flight Research Center Edwards, Calif., United States)