The use of flight tables and the present state of the art are described and the specifications for the flight table are derived. Major stress is laid on building a relatively cheap model, that will, nevertheless, satisfy the present requirements. A detailed description of the various alternatives that exist when deciding upon the major components is given along with a discussion on the linear design of the servo loops and stability validations for the expected nonlinearities. A grapho-analytical jump prediction is presented and the wiper backlash problem is analyzed.
A three-axis flight table with dc torque motors
IEEE TRANS. IND. ELECTRON. CONTROL INSTRUM. ; 18 , 4 ; 117-133
1971
17 Seiten, 23 Bilder, 11 Tabellen, 7 Quellen
Article (Journal)
English
EMPFINDLICHKEIT , FEHLER , FLUGSIMULATION , FREQUENZ , GLEICHSTROMMOTOR , KOPPLUNG , MESSUNG , MOMENT , SCHWELLENWERT , STABILITAET
NTRS | 1975
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