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Servo design and analysis of thrust vector control of launch vehicle

机译:运载火箭推力矢量控制的伺服设计与分析。

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Servo design includes the modelling of BLDC motor and to design a proper compensator to meet the launch vehicle requirements. Compensator design is based on step response of the open loop plant. A compensation scheme including PI controller and a notch filter is thus included in the plant to meet the plant requirements. Brush less torque motor, which is used as the actuator is used to control the engine. The system is closed using the compensator. From the step response of the closed loop system it is inferred that the system along with the compensation scheme is ready for thrust control of launch vehicles.
机译:伺服设计包括BLDC电机的建模,并设计合适的补偿器以满足运载火箭的要求。补偿器设计基于开环设备的阶跃响应。因此,包括PI控制器和陷波滤波器的补偿方案将包含在设备中,以满足设备要求。无刷扭矩电机,用作执行器来控制发动机。使用补偿器关闭系统。从闭环系统的阶跃响应可以推断,该系统连同补偿方案已准备就绪,可用于运载火箭的推力控制。

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