A Study of the Design of Acceleration Control System for Missiles

A Study of the Design of Acceleration Control System for Missiles

A 2-degrees of freedom PID controller is designed for a maneuvering acceleration control system. This design method is based on the combination of PID and IPD controller. Results show that (1) IP controller is superior to PI controller for the damper loop controller, (2) the selection of PI or IP co...

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Veröffentlicht in:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 2006, Vol.54(628), pp.228-231
Hauptverfasser: Kajita, Takanori, Eguchi, Hirofumi
Format: Artikel
Sprache:eng ; jpn
Schlagworte:
Acceleration Control System
Missile
PID/IPD Controller
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Zusammenfassung:A 2-degrees of freedom PID controller is designed for a maneuvering acceleration control system. This design method is based on the combination of PID and IPD controller. Results show that (1) IP controller is superior to PI controller for the damper loop controller, (2) the selection of PI or IP controller as for the acceleration controller depends on the tradeoffs between the responsibility and the reduction of inverse response.
ISSN:1344-6460
2432-3691
DOI:10.2322/jjsass.54.228