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UID:0-311@aerospace.technion.ac.il

DTSTART;TZID=Asia/Jerusalem:20191127T163000

DTEND;TZID=Asia/Jerusalem:20191127T173000

DTSTAMP:20230527T131722Z

URL:https://aerospace.technion.ac.il/events/performance-study-of-low-cost-
 rocket-controlled-by-solenoid/

SUMMARY:Performance Study of Low-Cost Rocket Controlled by Solenoid
DESCRIPTION:Lecturer:Benny Begun\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 Currently\, among aerospace industries\, there is an increa
 sing demand for advancements in rocket precision. Although these systems h
 ave provided great technological advancement in this arena\, they are acco
 mpanied by high costs and complex mechanisms.\nOne of the most common cont
 rol systems that are used in ammunition systems is the Servo. Despite its 
 common usage\, the mechanical complexity and high costs are of disadvantag
 e to aerospace industries.\nAs a result of the challenges associated with 
 the Servo system\, a considerable amount of research has been devoted to o
 btaining an alternative solution.\nThe main objective of the current resea
 rch is to propose a unique method to control a rocket which will strike th
 e balance between precise performances and the cost of the rocket.\nWe wil
 l begin the talk with an introduction and an overview of the current state
  concerning precise rockets. This will be followed by proposing a new guid
 ance law based on Vector Guidance law which leads to more robust rocket pe
 rformances while requiring low acceleration commands.\nAlso\, a unique act
 uating system driven by solenoids that are controlled by a PWM controller 
 will be shown.\nFinally\, the complete rocket configuration will be introd
 uced. Simulations results will be presented during the talk to exemplify t
 he results
CATEGORIES:Seminars
LOCATION:Classroom 165\, ground floor\, Library\, Aerospace Eng.

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