DocumentCode
585698
Title
Satellite positioning simulation system
Author
Pisolkar, Pranali ; Parmar, Sneha ; Poojari, Chitra ; Kalbande, Dhananjay
Author_Institution
Sardar Patel Inst. of Technol., Mumbai, India
fYear
2012
fDate
19-20 Oct. 2012
Firstpage
1
Lastpage
4
Abstract
A bangbang controller (on off controller), also known as a hysteresis controller, is a feedback controller that switches abruptly between two states. These controllers may be realized in terms of any element that provides hysteresis. They are often used to control a plant that accepts a binary input. With recent development of the space science and technology, higher requirements such as accuracy, robustness and disturbance rejection ability in satellite attitude control system have leaded to the more promising intelligent control methods. In order implement this artificial neural networks are a growing trend. A neural scheme of bang bang controller [1] is efficient in solving satellite orientation problems and also continuous updation of error. In control systems Fuzzy Inference Systems are used for loop control and to obtain desired output.
Keywords
aerospace computing; artificial satellites; attitude control; bang-bang control; control engineering computing; digital simulation; feedback; fuzzy reasoning; hysteresis; position control; robust control; bangbang controller; disturbance rejection ability; feedback controller; fuzzy inference systems; hysteresis controller; intelligent control methods; loop control; robustness; satellite attitude control system; satellite orientation problems; satellite positioning simulation system; space science; Aerospace electronics; Attitude control; Computers; Control systems; Learning; Satellites; Torque; Satellite attitude control; neuro-fuzzy control; reinforcement learning; temporal difference;
fLanguage
English
Publisher
ieee
Conference_Titel
Communication, Information & Computing Technology (ICCICT), 2012 International Conference on
Conference_Location
Mumbai
Print_ISBN
978-1-4577-2077-2
Type
conf
DOI
10.1109/ICCICT.2012.6398141
Filename
6398141
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