This work is concerned with the design of a pitch-rate-command-attitude-hold command and stability augmentation system in order that the augmented aircraft meets the Gibson dropback criterion, the Gibson phase-rate criterion ...
This work is concerned with the design of a pitch-rate-commandattitude-hold Command and Stability Augmentation System in order that
the augmented aircraft meets the Gibson dropback criterion, the Gibson
phase-rate criterion ...
This report describes a computer simulation model of the Boeing B-747 aircraft which is intended for use as a general purpose tool for research into advanced flight control systems for civil aircraft. The previously published ...