NASA NTRS · 19780028449
Adaptive control laws for F-8 flight test
Abstract
This paper describes an adaptive flight control system design for NASA's F-8 digital fly-by-wire research aircraft. This design implements an explicit parallel maximum likelihood identification algorithm to estimate key aircraft parameters. The estimates are used to compute gains in simplified quadratic-optimal command augmentation control laws. Design details for the control laws and identifier are presented, and performance evaluation results from NASA Langley's F-8 Simulator are summarized.
Keep this discovery
Explore connections, maps & timelines
Stein, G., Hartmann, G. L., Hendrick, R. C.. 1977-10-01. Adaptive control laws for F-8 flight test. https://ntrs.nasa.gov/citations/19780028449
Cite the original work for its findings. Save a collection to share your selection of sources.