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The high rolling speed of a missile heavily affects the stabilizing capability of the inertial platform in the laser tracking
system (LTS) of the missile. In this paper, a rotational stabilizing platform (RSP) and a fuzzy-PID controller is designed
to stabilize the inertial platform. This controller integrates the advantages of both fuzzy controller and classic PID controller.
A comparison study is carried out to illustrate the advantages of the proposed fuzzy-PID controller over the classic PID controller.
Numerical results indicate that the fuzzy-PID controller outperforms the classic one in effectively handling nonlinear disturbances
and quickly stabilizing the inertial platform at the sudden change of missile rolling speed.
Foundation item: the China Aerospace Science and Innovation Foundation (No. 06CASC0407) 相似文献
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