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- W2378284306 abstract "To solve the problem of critical stability or static instability caused by improving the maneuvering characteristics of guided-rockets,three control methods are researched,namely the mere rate-gyro-feedback-loop,the typical acceleration autopilot and the three-loop acceleration autopilot.The result indicates that the rate-gyro-feedback-loop alone makes the system stable but the damp-loop gain is too large to realize in engineering.The damp-loop gain of normal acceleration autopilot can be reduced greatly by introducing the acceleration-feedback.However,the rudder control surface bias will introduce system steady error.The three-loop autopilot not only makes stable for static unstable rocket stable but also it is insensitive to the rudder control surface bias.So the method of three-loop autopilot has priority in the guided-rocket control system." @default.
- W2378284306 created "2016-06-24" @default.
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- W2378284306 date "2010-01-01" @default.
- W2378284306 modified "2023-09-24" @default.
- W2378284306 title "Research on Guided-Rockets of Maneuvering Control System Design" @default.
- W2378284306 hasPublicationYear "2010" @default.
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