Attitude controller design of Hypersonic Vehicle using MPC

According to the Hypersonic Vehicle´s characteristics of strong uncertainty and multiple constraints, the 3-channel attitude controller is designed based on the continuous-time MPC method. Laguerre function is introduced while receding optimization, which turns regular optimization problem into optimization with LMIs. Simulation experiments are constructed on the 6-degree nonlinear model of some hypersonic vehicle. The simulation experimental results show that the performance of command tracking by this designed control system is quite good, especially under the condition of lacking of efficiency of control.