Problem considered is that of finding through use of observed data, coefficients of differential equations that describe dynamic system; problem occurs in determination of aerodynamic stability derivatives of airplane or missile from flight test data; free oscillation type of flight testing can never yield all coefficients; suitable forcing functions described do permit all coefficients to be evaluated.
Some basic concepts for analyzing dynamic flight-test data
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 20 , n 11
1953
9 pages
Aufsatz (Zeitschrift)
Englisch
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