The design of backstepping controller based on BTT missile
Shanzhong Liu, Ling Wei, Yongbin Liu
Abstract
Shanzhong Liu, Ling Wei, Yongbin Liu
Abstract
The performance of the controller is the key to ensure that the missile has a good stability and controllability in the guidance of flight. Without considering the coupling among channels, the three-channel missile body mathematical model of BTT-90 missile is established, and the model is based on BTT control technology. The Backstepping controller is designed and BTT-90 missile closed loop control system is constructed respectively. The result of simulation analysis shows that the control system can track the command signal rapidly, and has good dynamic and steady-state characteristics.
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The performance of the controller is the key to ensure that the missile has a good stability and controllability in the guidance of flight. Without considering the coupling among channels, the three-channel missile body mathematical model of BTT-90 missile is established, and the model is based on BTT control technology. The Backstepping controller is designed and BTT-90 missile closed loop control system is constructed respectively. The result of simulation analysis shows that the control system can track the command signal rapidly, and has good dynamic and steady-state characteristics.
Key concepts: Backstepping, Missile, Control theory (sociology), Controllability, Control engineering, Controller (irrigation), Computer science, Missile guidance