The report presents the results of a limited flight test investigation of pilot-induced oscillation (PIO) due to elevator rate limiting. The objective of this effort was to gather in-flight and ground-based simulation data on longitudinal PIO tendecies due to elevator rate limiting. Preliminary, ground-based simulation was conducted at the USAF Test Pilot School (TPS) from 1 March to 9 April 1997. Nine sorties, totaling 12.8 flight hours, were flown in the NT-33A aircraft. Additional ground-based simulation was conducted at the Flight Dynamics Directorate, Wright-Patterson AFB, Ohio, on 25 April 1997. The USAF TPS was the responsible test organization. File characteristics: Textfile. Physical description: 1 CD-ROM disc; System requirements: Windows; MSWORD.
Limited Flight Test Investigation of Pilot-Induced Oscillation Due to Elevator Rate Limiting (CD-ROM)
1997
1 pages
Report
Keine Angabe
Englisch
Job Training & Career Development , Aeronautics , Pilots , Man machine systems , Flight testing , Research aircraft , Handling , Data acquisition , Fly by wire control , Elevator rate limiting , Have limits , Pvt(Pilot vehicle interface) , Nt-33 aircraft , Pio(Pilot induced oscillation) , Multimedia(Cd- rom)
A Flight Investigation of Pilot-Induced Oscillation Due to Rate Limiting
British Library Conference Proceedings | 1998
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