Design of autopilot for Aerodynamic/Reaction-jet Multiple control missile using variable structure control

@article{Yonghua2008DesignOA,
  title={Design of autopilot for Aerodynamic/Reaction-jet Multiple control missile using variable structure control},
  author={Fan Yonghua and Li Xin and Yang Xiao Jun and Zhang Yuzhuo},
  journal={2008 27th Chinese Control Conference},
  year={2008},
  pages={642-645}
}
A switch scheme of reaction-jet/aerodynamic multi-control missile using pose controlled pulse-engine is present. In order to increase response speed of autopilot and reducing the coupling form Reaction-jet to aerohelm, in the last stage of attacking the aerodynamic controller is disconnection and Reaction-jet controller is used only. In the first part, the model of the Reaction-jet control system is given; then, the Reaction-jet controller has been designed by using variable structure control… CONTINUE READING

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