建立了运载器起飞段侧喷流直接力姿态控制模型。
A launch vehicle with lateral jet as its attitude control mechanism during ascending stage was proposed.
采用现代控制理论来设计气动力和姿控直接力子系统。
Modern control theory is applied to design the aerodynamics subsystem and the direct force subsystem.
直接力矩控制是交流调速中一种新颖、有效的控制方法。
The direct torque control (DTC) is a new, valid control strategy in AC drive.
对连接翼气动布局实现直接力控制的可能性进行了初步的探索。
This paper presents an approach to possibility of direct force control on the joined wing configuration.
最后，设计了移动质心与直接力复合控制动能弹的制导控制规律。
Finally, a design of the missile guidance control law is arrived at using proportional navigation method.
为飞机敏捷性、直接力控制和过失速机动问题提供了一种理论研究方法。
The study will provide a new theoretical approach to investigate aircraft agility, the direct force control and post-stall maneuver of modern combat aircraft.
本文为某型飞机设计了直接力两种模态——机身俯仰和垂直平移的控制器。
In the end of the paper, the controllers of pitch pointing and vertical translation modes are designed for an airplane. And the simulation results of two modes are excellent.
直接侧向力控制分为轨迹控制与姿态控制两种方式，本文研究姿态直接力控制。
The direct lateral force control includes two ways: trajectory control and position control. This research aims at lateral force control.
采用直接力控制可弥补常规飞机在轨迹操纵方面的不足，并产生某些新的运动模式。
The disadvantages of normal aircraft to realize flight path control can be overcome by using direct force control, and some new motion modes can be created.
采用直接力控制可弥补常规飞机在轨迹操纵方面的不足，并产生某些新的运动模式。
The disadvantages of normal aircraft in flight path control can be overcome by using direct force control, and some new motion modes can be realized.
为了提高直接力矩控制系统中定子磁链的观测精度，提出了一种新的定子磁链自适应观测器。
In order to improve the observing precision of the stator flux observer of DTC systems, a new adaptive stator flux observer is proposed.
点火控制算法基于极坐标的形式，该法可充分利用脉冲矢量发动机，且可灵活控制直接力的指向。
Ignition control algorithm is based on the polar coordinates, which can take full advantage of the motors, and regulate the direction of the direct force.
本文介绍了用于直接力矩控制系统的双cpu并行处理器，该系统的两片8098采用主—从工作方式。
In this paper, the author introduces the duplex Central Processing Unit (CPU) parallel system applied to the Direct Torque Control (DTC) system.
用该方法对某主动控制飞机的垂直平移模态（直接力控制）进行了解耦设计，并将其应用于飞机的阵风减缓。
As a numerical example, we used our method to design the vertical transition mode(direct lift control) of a certain active-control aircraft for gust alleviation.
介绍了直接力控制飞机的操纵品质判据——频带宽度，给出了频带宽度的定义和限制，讨论了频带宽度的机理。
This paper introduces the bandwidth—handling qualities criteria for direct force controlled aircraft, The definition and limitation of bandwidth is given.
文中基于广泛应用的比例导引律，对目标机动与导引指令信号进行分析，提出了一种直接力引入时机的设计方法。
Based on proportional navigation which is popularly used, target maneuver and guidance command is analyzed, and one design method of beginning time of reaction-jet is proposed.
用该综合方法对某型飞机的侧向直接力控制模态(航向指向)进行了分析与设计，并将其与动态逆方法进行了比较。
The design and simulation of the yaw pointing mode dynamic decoupling fuzzy control system for an aircraft are studied in this paper.
设计的轨控直接力作用于俯仰和偏航通道，而滚转通道没有直接力系统的作用，依靠气动舵面的偏转对滚转角进行稳定。
The direct force is acting on the pitch channel and the yaw channel, and the roll channel is stabilized by the fin surface deflection.
在飞行初段，提出用直接力来对弹道进行调姿以减小中制导段需用过载的方案，并利用最优控制的方法设计了直接力作用方案。
During the initial flight phase, the method which regulates the ballistic trajectory to reduce the overload requirement of the flight middle phase using the direct force is presented.
复合控制采用对制导指令进行前向分解的方法，将复合控制系统分为两个并行的子系统，即气动力控制子系统和直接力控制子系统。
By means of guidance command decomposed forwardly, the combined control system is divided into two parallel subsystems: the aerodynamics subsystem and the direct force subsystem.
复合控制采用对制导指令进行前向分解的方法，将复合控制系统分为两个并行的子系统，即气动力控制子系统和直接力控制子系统。
By means of guidance command decomposed forwardly, the combined control system is divided into two parallel subsystems: the aerodynamics subsystem and the direct force subsystem.
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