The problems concerning an aerospace vehicle's ( ASV) atmospheric reentry flight attitude control system were researched. 研究了空天飞行器(ASV)再入跨大气层飞行时的姿态控制问题。
Control and guide method for side window detection is studied, attitude control law of interceptor is given, and simulation test is done. 研究了侧窗探测条件下的制导控制技术,给出了拦截器的姿态控制规律,并进行了仿真。
Thrusters not responding. I've lost attitude control. 推进器没有用了,我无法控制。
The warhead attitude control system is one of the important parts of warhead control system for ballistic missiles, but it is difficult to optimize the system in design because of its nonlinearity. 弹头姿态控制系统是弹道导弹弹头控制技术的重要组成部分,但由于系统中明显包含非线性环节,所以造成设计时系统优化困难。
The liquefied gas propulsion system is a good selection for the micro satellite orbit and attitude control. 随着微小型卫星的发展,液化气推进系统成为了此类航天器推进系统的选择。
On the basis of this, an affine attitude dynamics model is established and the attitude control law is designed by using backstepping control method. 以此为基础,建立了仿射型姿态运动模型,利用退步方法设计了控制律;
To enhance the robustness of interceptor attitude control system, a switch control method is presented to control the attitude of interceptor. 为增强拦截器姿态控制系统的鲁棒性,提出了一种切换控制方法来控制拦截器的姿态。
Modeling and Simulation for Spacecraft Attitude Control System Considering Rotational and Flexible Accessories 考虑转动和挠性附件的航天器姿态控制系统建模与仿真
An image-based attitude control system for a space target simulator was presented. 提出了一种基于图像的空间目标器模拟装置的姿态控制系统。
In the end, we used the controller in the missile attitude control system, the simulation result shows that the controller has fine control effect and the performance can satisfy the requirements. 最后将所设计的控制律在导弹姿态控制系统中做了仿真应用,结果表明,所设计的控制器性能满足要求,控制效果较为满意。
This article deals with torque allocation for redundant flywheel configurations in a spacecraft attitude control system. 主要研究了航天器姿控系统中冗余飞轮构型的力矩分配问题。
Research and Simulation on the Effect of Excursion of Centroid on Attitude Control System 质心漂移对姿态控制系统影响的研究与仿真
The aerocraft attitude control is divided into two parts: attitude stabilization and attitude track. 本文将飞行器姿态控制分为:姿态稳定和姿态跟踪两种情况加以研究。
Research on Method of Spacecraft Attitude Control Based on Sliding Variable Structure 基于滑模变结构的航天器姿态控制方法研究
Flexible Spacecraft Attitude Control Design Based on Positive Real Method 基于正实性方法的挠性航天器姿态控制设计
Mass-shifting attitude control system 质量移动的姿态控制系统
The primary node is responsible for running the communications subsystems and the attitude control system code. 主要节点负责执行通讯子系统与姿态控制系统。
The attitude control problem of mass moment missile is analyzed from perspectives of both configuration and control law. 从构型和控制律设计两方面入手研究该类导弹跟踪控制问题。
In order to effectively adjust attitude motion of interceptor missile by combine control, an attitude control method was presented. 为了有效地调整复合控制拦截弹的姿态运动,提出了一个姿态控制方法。
Active satellite attitude control system 主动卫星姿态控制系统
Design for aerocraft attitude control system based on feedback-linearization and variable-structure-control 基于反馈线性化和变结构控制的飞行器姿态控制系统设计
Spacecraft attitude control based on inverse system and internal model 基于逆系统方法与内模原理的航天器姿态控制
Research on Attitude Control based on Virtual Reality Technology 基于虚拟现实技术的姿态控制应用研究
Reaction wheels are widely used in the modern spacecraft attitude control systems. 在现代卫星的姿态控制系统中,反作用轮得到了广泛应用。
Choosing the lateral accelerations of the missile as the output, the mathematical models of the attitude control system are constructed, analyzed and simplified. 以导弹的横向加速度为输出,建立了姿态系统数学模型,并对模型进行了分析和简化。
H_ ∞ Loop Shaping Design and Its Application to the Satellite Attitude Control H∞回路成形设计及其在卫星姿态控制中的应用
Application of Rigid Body Attitude Control in Gun's Automatic Aiming 刚体姿态控制在火炮自动操瞄中的应用
Reaction wheel is one of the main disturbance sources for the attitude control system accuracy of spacecraft. 反作用轮是影响航天器姿态控制系统精度的主要扰动源之一。
Dynamic Modeling and Attitude Control for Flexible Satellite 挠性卫星动力学建模与姿态控制研究
The integrated power and attitude control for a bias momentum attitude control system is investigated. 研究偏置动量姿态控制系统中的集成能量与姿态控制问题。