Simulink Modeling & Simulation Analysis of the Attitude ControlSystem on Three-channel of the Launch Vehicle
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Abstract:
Exampled by a certain launch vehicle, the modeling method and modelingprocess with Simulink to mathematicalsimulation on three-channel for the vehicle attitude control system are described.The problem of the local surge of the calculated data due to the so-called freeze time method during the simulation process is analyzed and the resolvent is given. Algebraic loop problem encounteredinSimulinkmodeling of this large scale system is discussed and the resolvent is given.
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SUN Zhibing, DAI Jinhai. Simulink Modeling & Simulation Analysis of the Attitude ControlSystem on Three-channel of the Launch Vehicle[J]. Journal of National University of Defense Technology,2004,26(3):20-23.