针对单轴定向大气层外拦截器设计了一种姿态控制律。
An attitude control law for single axial direction control of an exoatmospheric interceptor is put forward.
为研究具有大离轴角及越肩发射能力的先进空空导弹初始段敏捷转弯方法，研究了装有反作用喷气控制系统的空空导弹的大角度姿态过失速机动控制律。
This paper investigates the large Angle attitude post stall maneuver control for the agile turn phase of an air-to-air missile that has high off-boresight capability and head reverse maneuverability.
文中通过研究无人机纵向航迹跟踪和横侧向协调转弯的控制律使得无人机可以以下确的姿态沿预定的航迹飞行。
The UAV can fly along the scheduled fight path with correct attitude by the research of the control law of portrait flight track and transverse coordinated turn.
以一个呈现混沌姿态运动的航天器动力学模型为例说明了该控制律的应用。
A mathematical model derived from spacecraft attitude dynamics is treated as an example to demonstrate its application.
采用输出变量反馈线性化控制律及其局部线性化将混沌姿态运动控制为给定的静止状态和周期运动。
The input_output feedback linearization method and its modified version are respectively applied to control chaotic attitude motions to the given attitude rest and the periodic motion.
该变结构控制律在实现姿态控制系统鲁棒控制的同时，有效地抑制了传统变结构控制的抖振现象。
This VS control law implements robust control of attitude control system, at the same time, it overcomes the traditional chattering problem.
该变结构控制律在实现姿态控制系统鲁棒控制的同时，有效地抑制了传统变结构控制的抖振现象。
This VS control law implements robust control of attitude control system, at the same time, it overcome the chattering problem.
理论分析和仿真研究表明此控制律具有姿态跟踪精度高，实时计算量小，便于工程实现等优点。
Theoretical analysis and the simulation results show that this method has the advantages of good attitude tracking accuracy, less real time calculations and easy realization.
采用输出变量反馈线性化控制律及其局部线性化将混沌姿态运动控制为给定的静止状态和周期运动。
The input_output feedback linearization method and its modified version are respectively applied to control chaotic attitude motions t.
首先建立了以变速控制力矩陀螺为执行机构的航天器姿态动力学模型，并给出了全局稳定的姿态反馈控制律。
The attitude dynamic equation of a spacecraft with VSCMG attached and a global asymptotical attitude feedback control law are presented firstly.
本文对猎雷艇声纳基阵俯仰角姿态伺服系统分别进行了领域法控制律的设计和变结构控制律的设计。
The design of servo system for pitch attitudes of a mine hunting sonar array was made using frequency domain control and variable structure control respectively.
退步控制是一种有效设计级联系统控制律的方法，而基于单位四元数的刚体姿态方程就是一种典型的级联系统。
Backstepping control scheme was an effective way to design control laws of a cascade system. Quaternion-based attitude equations of a rigid body was a typical cascade system.
当诊断出故障时，重构控制律的参数对系统进行补偿控制，使得故障下飞行器的姿态跟踪精度得以维持。
Once a fault is detected and isolated, controller parameters can be reconfigured to compensate the loss of performance and keep the good attitude tracking accuracy of the spacecraft.
当诊断出故障时，重构控制律的参数对系统进行补偿控制，使得故障下飞行器的姿态跟踪精度得以维持。
Once a fault is detected and isolated, controller parameters can be reconfigured to compensate the loss of performance and to keep the good attitude tracking accuracy of the spacecraft.
研究航天器集成能量与姿态控制系统中飞轮的控制律。
Research on Distributed Interactive Simulation Method of Missiles Attitude Control System;
研究航天器集成能量与姿态控制系统中飞轮的控制律。
Research on Distributed Interactive Simulation Method of Missiles Attitude Control System;
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