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UID:0-448@aerospace.technion.ac.il

DTSTART;TZID=Asia/Jerusalem:20161130T163000

DTEND;TZID=Asia/Jerusalem:20161130T173000

DTSTAMP:20230603T190315Z

URL:https://aerospace.technion.ac.il/events/full-state-autopilot-guidance-
 for-multi-input-multi-output-missile-engagements/

SUMMARY:Full-State Autopilot & Guidance for Multi-Input  Multi-Output Missi
 le Engagements
DESCRIPTION:Lecturer:Maital Levy\n Faculty:Department of Aerospace Engineer
 ing\n Institute:Technion – Israel Institute of Technology\n Location:Cla
 ssroom 165\, ground floor\, Library\, Aerospace Eng.\n Zoom: \n Abstract: 
 \n Details: \n There are two main approaches to design autopilot and guida
 nce systems: “Single-Loop” and “Two-Loop”. In the “Single-Loop
 ” approach there is no definite autopilot\, and the guidance command is 
 applied directly to the actuators. In the “Two-Loop” approach the inne
 r autopilot loop has to follow commands generated by the outer guidance lo
 op\, and each loop is designed separately. The main goal of the research w
 as to identify the merits of each approach\, and combine the benefits of t
 he two approaches into a new improved one.\nIn the talk\, the advantages o
 f the “Two-Loop” and “Single-Loop” approaches will be discussed. T
 he conditions for obtaining equivalence between the two design approaches 
 will be presented. Broadly speaking\, an equivalence relation between thes
 e two design approaches holds if full-state feedback exists and the number
  of guidance commands is equal to the number of available controls. The eq
 uivalence conditions are established under linear quadratic optimal contro
 l and differential game formulations\, and for nonlinear systems with boun
 ded controls. The performance of the “Two-Loop” and “Single-Loop” 
 approaches to design autopilot and guidance systems is illustrated via sim
 ulations.
CATEGORIES:Seminars
LOCATION:Classroom 165\, ground floor\, Library\, Aerospace Eng.

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DTSTART:20161030T010000

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