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UID:0-410@aerospace.technion.ac.il

DTSTART;TZID=Asia/Jerusalem:20171023T163000

DTEND;TZID=Asia/Jerusalem:20171023T173000

DTSTAMP:20230530T180452Z

URL:https://aerospace.technion.ac.il/events/seminar-in-memory-of-prof-shmu
 el-and-mrs-noemi-merhav-full-state-autopilot-guidance-for-multi-input-mult
 i-output-missile-engagements/

SUMMARY:Seminar in Memory of Prof. Shmuel and Mrs. Noemi Merhav – Full-St
 ate Autopilot & Guidance for Multi-Input Multi-Output Missile Engagements
DESCRIPTION:Lecturer:Dr. Maital Levy\n Faculty:Department of Aerospace Engi
 neering\n Institute:Technion – Israel Institute of Technology\n Location
 :Classroom 165\, ground floor\, Library\, Aerospace Eng.\n Zoom: \n Abstra
 ct: \n Details: \n There are two main approaches to design autopilot and g
 uidance systems: “Single-Loop” and “Two-Loop”. In the “Single-Lo
 op” approach there is no definite autopilot\, and the guidance command i
 s applied directly to the actuators. In the “Two-Loop” approach the in
 ner autopilot loop has to follow commands generated by the outer guidance 
 loop\, and each loop is designed separately. The main goal of the research
  was to identify the merits of each approach\, and combine the benefits of
  the two approaches into a new improved one.\n\nIn the talk\, the advantag
 es of the “Two-Loop” and “Single-Loop” approaches will be discusse
 d. The conditions for obtaining equivalence between the two design approac
 hes will be presented. Broadly speaking\, an equivalence relation between 
 these two design approaches holds if full-state feedback exists and the nu
 mber of guidance commands is equal to the number of available controls. Th
 e equivalence conditions are established under linear quadratic optimal co
 ntrol and differential game formulations\, and for nonlinear systems with 
 bounded controls. The performance of the “Two-Loop” and “Single-Loop
 ” approaches to design autopilot and guidance systems is illustrated via
  simulations.
CATEGORIES:Seminars
LOCATION:Classroom 165\, ground floor\, Library\, Aerospace Eng.

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