A technique is proposed which will make the flight director computer performance independent of aircraft dynamics, wind or aircraft position relative to the navigation beam. The control law proposed will compensate for all such variables with an error correcting mechanism. This technique results in a computer that is universal in its application.
A Universal Flight Director Computer
1974
60 pages
Report
Keine Angabe
Englisch
A universal flight director computer (final rept.)
Tema Archiv | 1974
|Digital Flight Director Computer
NTIS | 1975
|SAE Technical Papers | 1991