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IEEE5d
Design & development of a simulation system for ballistic missile
Abstract: The computation of the positioning and launching parameters wrt time, for missile system is done by the interface unit called Intercept missile unit (IMU) controlled by computer.When the ...
World Scientific6d
Dynamic surface control and active disturbance rejection control-based integrated guidance and control design and simulation for hypersonic reentry missile
State Key Laboratory of Virtual Reality Technology and Systems, Beihang University, Beijing 100191, P. R. China School of Automation Science and Electrical Engineering, Beihang University, Beijing ...