On one test system, it resulted in a 22% speed increase on a test program with a tight inner loop .
在一个测试系统上，对一个有紧内部循环的程序，它的执行结果有22%的速度提升。
The control laws of the inner closed loop system and post stall maneuver are obtained through using symbol operations design.
使用符号运算方法设计了系统闭环控制律和大攻角下的过失速控制律。
Proportional controller can be adopted concerning the fast response of inner loop. Thus the design of whole system is very simple.
考虑内环的快速性，外环可以采用简单的比例调节器，从而整个数字双环控制系统的设计非常简单。
Then, this thesis applies IP control algorithm to change controller in outer loop but not in inner loop based on basic double closed loop control system.
然后，本文在传统双闭环控制的基础上，内环的控制算法不变，改变外环控制器的设计算法，主要采用IP控制方案。
According to all of these characteristics of the system, a three-loop fuzzy sliding control mode is adopted, the speed and position loop are outer loop, and the current loop is inner loop.
根据系统这一特点，采用三闭环模糊滑模控制策略，外环为速度和位置闭环，内环为电流闭环的方法设计控制器，并进行了仿真实验研究。
Two closed loops are constructed in the control system; the inner loop is currentfeedback that is to adjust the torque of the motor.
系统采用双闭环控制，内环采用电流负反馈对电机转矩进行调节；
The system has retained the advantages of traditional cascade control systems, which consist of overcoming inner-loop disturbances and increasing the working frequency of the system.
系统保留了传统串级控制系统克服内回路扰动、提高系统工作频率的优点。
Flywheel control system has two closed loops, the inner is voltage stabilization loop, other is current loop or is speed loop in different mode.
飞轮控制系统是个多回路系统，内回路为电压稳定回路，外回路在不同的工作模式下分别为电流回路和转速回路。
The capacitive current inner loop is used to suppress system instability and the capacitive current is obtained by estimation.
算法引入电容电流内环以抑制系统不稳定的现象，电容电流信号通过估计过程得到。
The spacecraft's attitude control system was divided into the outer loop that was Angle loop and the inner loop that was Angle velocity loop based on their time scales.
基于奇异摄动思想，将飞行器姿态控制系统分为慢变化的姿态角回路和快变化的角速度回路分别设计。
The aerocraft's attitude control system is divided into the outer loop that is an Angle loop and the inner loop that is an Angle velocity loop based on their timescale separation principle.
基于时标分离思想，将飞行器姿态控制系统分为慢变化的姿态角回路和快变化的角速度回路分别设计。
The control system is made of double closed loops: the inner current loop and the outer temperature loop, and satisfies the EAF's temperature need and three phase current balance.
采用温度控制外环和电流平衡控制内环的双闭环结构实现电弧炉温度和电极三相电流平衡的智能集成控制。
The ADS1110 was used to feed back output signals to MCU, and a double-loop regulation system with analog inner-loop and digital outer-loop was formed.
并以ADS1110将输出信号反馈到单片机，形成模拟内环和数字外环的双闭环调节系统。
The controller studied in this paper is based on cascade control system. Intelligent fuzz control is used to the outer loop and traditional PID law is applied to the inner loop.
在串级控制系统的基础上，主调节器采用智能模糊PID控制算法，副调节器采用常规PID算法。
Outer inner voltage-current dual closed loop control system to improve the system accuracy and stability of the output and improve the system dynamic response.
采用电压外环电流内环双闭环控制系统，提高了系统的输出的精度和稳定性，改善了系统动态响应特性。
For TD-SCDMA system, the closed-loop power control(PC)consists of inner-loop PC and outer-loop PC.
SCDMA系统的闭环功率控制可以分为外环功控和内环功控。
Inner-loop control for quick system respondence for changes in Arc length are constantly;
采用内环特性控制；系统响应速度快，能迅速响应弧长变化，不断弧；
Inner-loop control for quick system respondence for changes in Arc length are constantly;
采用内环特性控制；系统响应速度快，能迅速响应弧长变化，不断弧；
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