- F-16 Model:
Back in november there was some discussion about an F-16 Model for high angle of
attack simulation. While browsing the NASA Langley tech report server today, I
stumbled across 2 interesting documents: 1.) the much cited 1979 "F16" report
TP-1538 (used by Stevens/Lewis) is available on the web (= 31 MB !!). The report
includes the full data table, and analysis of simulator flight and control laws
for pitch, roll and yaw axis. However, be warned that these control laws might
not really be related to the "real" control laws used on the production aircraft.
One of the interesting things of the F-16 is that it rolls around it's velocity vector rather than the body axis to prevent high AOA to go into a large sideslip.
This should be a challenge to model ...
Erik
BTW. Thanks for the message, it's quite educative.
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