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SUMMARY:Stabilizing an aircraft on a previously calculated trajectory
DTSTART:20130513T103000
DTEND:20130513T113000
DTSTAMP:20260408T052739Z
UID:b812329df434214432df8f213ac21874f82ab845da0a2c616d755ce5
CATEGORIES:Conferences - Seminars
DESCRIPTION:Ekaterina Fokina\nAn algorithm for an aircraft autopilot syste
 m was developed and optimized. The diploma project consists of the followi
 ng parts: research\, engineering\, technology\, economy and ecology. In th
 e research part an algorithm was developed to generate the best trajectory
  for an aircraft to reach a designated altitude within minimum time. The r
 equired aerodynamic coefficients were calculated. From the calculated poin
 ts in the flight area the optimal trajectory of the aircraft was derived. 
 The structural control schemes of the autopilot with different control law
 s\, corresponding to different flight modes on the trajectory of interest\
 , were examined.\nIn the engineering part a steering control unit (SCU) wa
 s designed and the necessary calculations were carried out. The SCU assemb
 ly process was developed in the technological part. Indicators of technolo
 gical design were calculated in order to assess the quality of the SCU.\nI
 n the organizational part\, the different stages of the research are liste
 d and described. In the economic part\, the labor intensity of the researc
 h\, technological and engineering parts is calculated. Regarding industria
 l ecology and industrial safety\, the dangerous and harmful factors concer
 ning work with a PC were analyzed.
LOCATION:PPB 019
STATUS:CONFIRMED
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