The simulation requirements for investigation of pilot-induced-oscillation (PIO) characteristics during the landing phase are discussed. Orbiters simulations and F-8 digital fly-by-wire aircraft tests are addressed.
Space Shuttle Pilot-Induced-Oscillation Research Testing
1984
10 pages
Report
Keine Angabe
Englisch
Space shuttle pilot-induced-oscillation research testing
NTRS | 1984
|Space shuttle avionics testing
Tema Archiv | 1977
|Improved Pilot Model for Space Shuttle Rendezvous
Online Contents | 1997
|