Research on the Composite Control Over Gas-Flotage Cross Beam Experiment System Based on Reaching Law Sliding Mode Control
Yue Zhi · Journal of Naval Aeronautical and Astronautical University · 2008
The three degrees of freedom dynamic equation of gas-flotage crossbeam with double operators based on composite control of aerodynamics-mass moment was derived. A sliding mode variable structure controller based on reaching law was designed in this paper. Simulation and practicality experiment about the crossbeam attitude confined to vertical plane was performed, which laid a foundation on developing the composite control of aerodynamics-mass moment control.