Title :
A graphical design methodology of missile autopilot
Author :
Pain, S. ; Tiwari, Kamlesh
Author_Institution :
Dept. of Appl. Electron. & Instrum. Eng., Dr. B.C. Roy Eng. Coll., Durgapur, India
Abstract :
The graphical design methodology for designing two loop lateral missile autopilot has been proposed. The design methodology enables to find out graphically maximum attainable autopilot gain cross over frequency and the corresponding set of control gains. This method may be used to choose the possible phase margin and gain margin pairs and feasibility of obtaining the control gains for any user specifications on phase margin and gain margin. The step by step design algorithm has been given in detail and illustrated with one numerical example.
Keywords :
design engineering; missile control; control gains; gain margin pairs; graphical design methodology; loop lateral missile autopilot design; maximum attainable autopilot gain cross over frequency; phase margin; Actuators; Design methodology; Equations; Frequency control; Frequency locked loops; Gain; Missiles; Two loop autopilot; control gain; fin servo gain; graphical technique; missile;
Conference_Titel :
Automation, Computing, Communication, Control and Compressed Sensing (iMac4s), 2013 International Multi-Conference on
Conference_Location :
Kottayam
Print_ISBN :
978-1-4673-5089-1
DOI :
10.1109/iMac4s.2013.6526490
