Flight testing of the Space Shuttle Orbiter is in progress and current results of the post-flight aerodynamic analyses are discussed. The purpose of these analyses is to reduce the pre-flight aerodynamic uncertainties, thereby leading to operational certification of the Orbiter flight envelope relative to the integrated airframe and flight control system. Primary data reduction is accomplished with a well documented maximum likelihood system identification techniques.
Stability and control flight test results of the space transportation system's orbiter
Atmospheric Flight Mechanics Conference ; 1982 ; San Diego, CA
1982-08-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
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