A multi-objective design optimization procedure for a general control system


Makaraci M.

7th International Conference and Exposition on Engineering, Construction, Operations, and Business in Space, New Mexico, Amerika Birleşik Devletleri, 27 Şubat - 02 Mart 2000, ss.377-383 identifier identifier identifier

  • Yayın Türü: Bildiri / Tam Metin Bildiri
  • Doi Numarası: 10.1061/40479(204)45
  • Basıldığı Şehir: New Mexico
  • Basıldığı Ülke: Amerika Birleşik Devletleri
  • Sayfa Sayıları: ss.377-383
  • Kocaeli Üniversitesi Adresli: Evet

Özet

With the advancement in new materials and techniques, smooth and high performance operation of critical systems, such as flight simulators, satellite navigators and robot arms, are expected. To give examples, a long duration for space shuttle after its take off cannot be tolerated in terms of its system dynamics and stability as well as high off-the-target position errors for a pick-and-place robot. In most of these military and industrial systems, control objectives are more than one and mostly intensified at minimizing overshoot from steady state response with a minimum system settling time. Stability of the systems is also another objective.