BTT and STT Control BTT与STT控制
The features of the BTT control method determine that its mathematical model contains many coupling elements, such as kinematical coupling, aero dynamical coupling, inertial coupling etc.
BTT飞行的特点决定了控制系统存在着运动学耦合、气动耦合和惯性耦合等多种耦合因素。
Focused on the problem of reusable launch vehicle (RLV) attitude control, an engineering attitude control system based on the classical control theory and BTT technology was designed.
基于古典控制理论和BTT倾斜转弯控制技术，设计了可重复使用运载器(RLV)的大气层内姿态稳定控制系统。
Based on the law that the sliding mode of variable structure control is constant to external interference, the thesis designed the output decoupling law of BTT missile.
本文在变结构控制理论对外界扰动的不变性原理的基础上，采用变结构控制方法设计了BTT导弹的输出解耦控制律。
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