NASA NTRS · 19780021159
Propulsion/flight control integration technology (PROFIT) software system definition
Abstract
The Propulsion Flight Control Integration Technology (PROFIT) program is designed to develop a flying testbed dedicated to controls research. The control software for PROFIT is defined. Maximum flexibility, needed for long term use of the flight facility, is achieved through a modular design. The Host program, processes inputs from the telemetry uplink, aircraft central computer, cockpit computer control and plant sensors to form an input data base for use by the control algorithms. The control algorithms, programmed as application modules, process the input data to generate an output data base. The Host program formats the data for output to the telemetry downlink, the cockpit computer control, and the control effectors. Two applications modules are defined - the bill of materials F-100 engine control and the bill of materials F-15 inlet control.
Keep this discovery
Explore connections, maps & timelines
Carlin, C. M., Hastings, W. J.. 1978-07-01. Propulsion/flight control integration technology (PROFIT) software system definition. https://ntrs.nasa.gov/citations/19780021159
Cite the original work for its findings. Save a collection to share your selection of sources.