飛翔体旋回加速度制御系設計に関する一考察 [in Japanese] A Study of the Design of Acceleration Control System for Missiles [in Japanese]
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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.
- JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 54(628), 228-231, 2006-05-05
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES