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UID:0-436@aerospace.technion.ac.il

DTSTART;TZID=Asia/Jerusalem:20170503T163000

DTEND;TZID=Asia/Jerusalem:20170503T173000

DTSTAMP:20230530T181104Z

URL:https://aerospace.technion.ac.il/events/thrust-inclination-guidance-an
 d-control/

SUMMARY:Thrust Inclination Guidance and Control
DESCRIPTION:Lecturer:Prof. Shaul Gutman\n Faculty:Department of Mechanical 
 Engineering\n Institute:Technion – Israel Institute of Technology\n Loca
 tion:Classroom 165\, ground floor\, Library\, Aerospace Eng.\n Zoom: \n Ab
 stract: \n Details: \n In exo-atmospheric guidance the control is the thru
 st vector. A recent thrust vector approach has revealed that in optimal gu
 idance the thrust inclination in an inertial frame is constant. Thus\, in 
 this talk\, the usual acceleration vector command is replaced by the thrus
 t inclination scalar command. An autopilot that keeps the thrust inclinati
 on constant completes the guidance loop. The guidance law is based on the 
 range\, Line-Of-Sight (LOS) angle\, and their derivatives. This is done wi
 thout kinematics linearization. Simulations demonstrate the overall perfor
 mances.
CATEGORIES:Seminars
LOCATION:Classroom 165\, ground floor\, Library\, Aerospace Eng.

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