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Erschienen in:
2012 | OriginalPaper | Buchkapitel
Analysis for Height Control-Loop of Cruise Missile to Different Kinds of Autopilot
verfasst von : Qiuqiu Wen, Qunli Xia, Chuntao Cai
Erschienen in: Advances in Automation and Robotics, Vol. 2
Verlag: Springer Berlin Heidelberg
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The models of two kinds of height control system which include the attitude autopilot inner loop and acceleration autopilot inner loop respectively are built. The response rate, stabilization and engineer realization of gravity compensation of the height control systems are analyzed and compared. The result shows that they have same performances and can be used both in missile altitude control. The gravity compensation can improve the transition quality of height control and decrease the overshoot. The gravity compensation command matching attitude autopilot depends on the flying parameter heavily, so the engineer reliability is lower than acceleration autopilot.