Backup flight control system for a highly maneuverable remotely piloted research vehicleNASA is currently conducting flight tests of a remotely piloted subscale advanced fighter configuration as part of the Highly Maneuverable Aircraft Technology (HiMAT) program. This paper describes the initial development, user modification, and flight test experience of a back-up control system (BCS) contained within one of two onboard microprocessors. The development of the BCS proceeded in two distinct steps: the initial contractor development of control laws and logic to satisfy BCS design objectives, and user modifications required to satisfy operational requirements. A brief resume of flight qualification procedures and pilot comments is presented.
Document ID
19800061378
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Hoyt, C. E. (Teledyne Ryan Aeronautical San Diego, Calif., United States)
Kempel, R. W. (Teledyne Ryan Aeronautical Co. San Diego, CA, United States)
Larson, R. R. (NASA Headquarters Washington, DC United States)