Comparison of numerical solution of longitudinal motion with flight test data is presented for piloted aircraft dropping heavy loads; procedure causes wide variation of aircraft dynamic characteristics, partially in unstable region; relatively simple "human pilot model" is shown to be adequate for good prediction of in-flight aircraft behavior, in spite of generally complicated case; numerical solution presents considerable difficulties, which arise in many of usual integration methods; special method for solution was developed, which will also be applicable to other types of " pilot's equations".
Investigation of longitudinal dynamics of piloted aircraft during rapid dropping of concentrated loads
Israel J Technology
Israel Journal of Technology ; 4 , n 1
1966
8 pages
Aufsatz (Zeitschrift)
Englisch
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