A Study on Missile Reentry Control Based on the Method of Feedback Linearization

摘要

In the process of missile large attack angle reentry, there exist nonlinear, strong coupling uncertainty and multi-input—multi-output (MIMO) in the movement equations, so the traditional small disturbance faces difficulties. For such situations, the method of feedback linearization is adopted to control the complex system, and the control method based on the fuzzy adaptive nonlinear dynamic inversion decoupling control of missile is proposed in the paper. According to the principle of time-scale separation, the system is separated into fast loop and slow loop, the method of dynamic inversion is applied to them, and the method of adaptive fuzzy approach is adopted to compensate for the uncertainty of the fast loop. The simulation results denote the control method in the paper has a better tracing characteristic and robustness.