The NASA Dryden Flight Research Center has completed the initial flight test of a modified set of F/A-18 flight control computers that gives the aircraft a research control law capability. The production support flight control computers (PSFCC) provide an increased capability for flight research in the control law, handling qualities, and flight systems areas. The PSFCC feature a research flight control processor that is "piggybacked" onto the baseline F/A-18 flight control system. This research processor allows for pilot selection of research control law operation in flight. To validate flight operation, a replication of a standard F/A-18 control law was programmed into the research processor and flight-tested over a limited envelope. This...
The Integrated Test Facility, built at the NASA Dryden Flight Research Facility, provides new real-t...
The Active Aeroelastic Wing research program was a joint program between the U.S. Air Force Research...
This paper describes the design, development, and ground testing of the propulsion controlled aircra...
NASA Dryden Flight Research Center (DFRC) is working with the United States Navy to complete ground ...
The NASA Dryden Flight Research Center has been conducting integrated flight-propulsion control flig...
Hardware and software design of the performance seeking control (PSC) for the NASA F-15 research air...
This report documents the updated performance characteristics of NASA Langley Research Center's (LaR...
Flight research for the F-15 HIDEC (Highly Integrated Digital Electronic Control) program was comple...
A NASA program to develop digital fly-by-wire (DFBW) technology for aircraft applications is discuss...
Research on flight control systems is reviewed. Investigations were conducted to evaluate and test a...
New flight test techniques in use at Ames Dryden are reviewed. The use of the pilot in combination w...
Successful flight-testing of the Active Aeroelastic Wing airplane was completed in March 2005. This ...
A flight simulation program was conducted on the flight simulator for advanced aircraft (FSAA). The ...
Automated validation of flight-critical embedded systems is being done at ARC Dryden Flight Research...
A flight test evaluation of the digital elctronic engine control (DEEC) system was conducted. An ove...
The Integrated Test Facility, built at the NASA Dryden Flight Research Facility, provides new real-t...
The Active Aeroelastic Wing research program was a joint program between the U.S. Air Force Research...
This paper describes the design, development, and ground testing of the propulsion controlled aircra...
NASA Dryden Flight Research Center (DFRC) is working with the United States Navy to complete ground ...
The NASA Dryden Flight Research Center has been conducting integrated flight-propulsion control flig...
Hardware and software design of the performance seeking control (PSC) for the NASA F-15 research air...
This report documents the updated performance characteristics of NASA Langley Research Center's (LaR...
Flight research for the F-15 HIDEC (Highly Integrated Digital Electronic Control) program was comple...
A NASA program to develop digital fly-by-wire (DFBW) technology for aircraft applications is discuss...
Research on flight control systems is reviewed. Investigations were conducted to evaluate and test a...
New flight test techniques in use at Ames Dryden are reviewed. The use of the pilot in combination w...
Successful flight-testing of the Active Aeroelastic Wing airplane was completed in March 2005. This ...
A flight simulation program was conducted on the flight simulator for advanced aircraft (FSAA). The ...
Automated validation of flight-critical embedded systems is being done at ARC Dryden Flight Research...
A flight test evaluation of the digital elctronic engine control (DEEC) system was conducted. An ove...
The Integrated Test Facility, built at the NASA Dryden Flight Research Facility, provides new real-t...
The Active Aeroelastic Wing research program was a joint program between the U.S. Air Force Research...
This paper describes the design, development, and ground testing of the propulsion controlled aircra...