System uses identification and synthesis processes to determine what changes in control parameters are required to adapt to changes in dynamics of vehicle as it experiences wide range of flight conditions; identification of vehicle dynamics is accomplished by improved identification technique; digital computer simulation of digital adaptive pitch rate flight control system was performed which included identification of fourth-order aerospace vehicle and actuation system and synthesis of fourth-order digital compensator.
Digital adaptive flight control system for aerospace vehicles
AIAA J
AIAA Journal ; 1 , n 5
1963
5 pages
Aufsatz (Zeitschrift)
Englisch
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