Block Diagonal Control for Bank to Turn Winged Missile

摘要

The Theory of Block Diagonal Control (BDC) is applied to Bank to Turn (BTT) winged missile. The analytic inverse solutions of equations of the BTT missile are given. The BDC flight control system is constructed. To check the performance of the designed BDC control system, Six Degree Of Freedom (6DOF) mathematical simulation is conducted. Simulation results show that the designed BDC can control the BTT missile stably and accurately.