Research Progress on Design Methods for Missile Integrated Guidance and Control
2017
The design for missile integrated guidance control is to combine the missile guidance and control circuit into one loop. According to the relative motion of the missile and target, the control command is directly obtained to further improve the guidance and control precision. This paper summarizes the domestic and foreign research progress on the design methods of missile integrated guidance control in recent years, studies and summarizes its advantages and disadvantages, and analyzes the main problems and development trend of missile integrated guidance and control design.
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