自旋稳定

自旋稳定静止卫星热设计中若干问题的探讨

Research on several problems in thermal design for spin-stabilized geostationary satellite

自旋稳定卫星同步控制时延计算与应用策略研究

Strategies of Calculating and Applying the Time Delay to Control Spin-Stabilized Satellites Synchronously

自旋稳定卫星姿态参数的容错Kalman滤波

Fault-Tolerant Kalman Filter for Attitude Parameters of the Spin Stabilized Satellite

自旋稳定卫星姿态参数递推容错LS估计

Recursive Fault-Tolerant LS Estimation for Attitude Parameters of a Spin Stabilization Satellite

ESR自旋稳定化技术在漆酶化学中的应用

The application of ESR-spin Stable Technique in Laccase Chemical System

运载火箭的自旋稳定问题考虑热解反应的阴燃渐近分析

SPIN STABILIZATION OF SATELLITE-LAUNCHER UPSTAGE Asymptotic analysis of steady reverse smolder

自旋稳定静止气象卫星扫描辐射计水汽通道外定标方法研究

The vicarious calibration for water vapor channel of spin stabilization geostationary meteorological satellite

半充液自旋稳定卫星的一个实验模型

A Test Model of Spinning-Satellites with Partially Liquid-Filled Tanks

自旋稳定通信卫星姿态确定的矩阵方法

Matrix method of attitude for spin-stabilized geostationary communication satellite

月球探测技术&奔月变轨过程自旋稳定指向控制

Technology of the Moon Exploration & Orientation Control for Lunar Probe during Translunar Injection

大气层外自旋稳定拦截器末制导控制研究

Terminal Guidance Study of Exoatmospheric Spin Stabilized Interceptor

一种对自旋稳定目标的判别方法

A Method for Recognition of Spin Stabilization Targets

自旋稳定动能拦截器轨控发动机推力控制

Thrust Control for Spin-Stabilized Kinetic Kill Vehicle

利用落塔试验研究液体晃动对卫星自旋稳定的影响。

The effects of liquid sloshing on spinning stability of satellite are investigated by means of drop test .

本论文主要针对具有自旋稳定特征目标进行成像算法及运动补偿的研究。

In this thesis the radar imaging algorithm and motion compensation to the spinning target is discussed particularly .

本文讨论卫星运载火箭末级自旋稳定问题，分析了干扰因素的影响。

This papar presents preliminary assessment about spin stabilization of satellite-launcher upstage and analyses the influence of the interference factors .

自旋稳定卫星的动力学特征决定了对其控制时必须采用同步控制方式。

Because of the dynamics characteristics of the spin stabilized satellites , the synchronous control mode is used to control this kind of satellites .

文章陈述了自旋稳定通信卫星姿态确定的矩阵方法及其工程应用的七种情况。

The matrix method of the attitude determination for spin-stabilized geostationary communication satellite and its cases of practical engineering application are described in this paper .

以科学双星计划中两个自旋稳定的小卫星为背景，介绍了在双星运行轨道所受到的空间干扰力矩情况；

Based on the two spin satellites in the Double-Star project , the on-orbit disturbing torques on the two satellites are presented in this paper .

最后，设计了自旋稳定拦截器制导仿真平台。

The simulation results showed the validity and superiority of this fire algorithm . Finally , the guidance simulation platform of spinning mini-interceptor was designed .

其次针对目标的特殊性，总结了各种运动补偿方式，归纳改进了适合自旋稳定目标成像的包络对齐及相位校正的算法。

Secondly , many motion compensation methods are compared and improved including range alignment and phase correction in order to satisfy various targets imaging conditions .

自旋稳定固体火箭发动机飞行器随着发动机尺寸的增大，工作时间的增长，在发动机工作末期出现了不可预见的不稳定性运动。

As the increase of motor size and the time of motor operation , the spin stabilized solid rocket propelled space vehicles performed the unpredictable nutation instability .

风云二号自旋稳定地球同步气象卫星，以地球脉冲作为姿态控制基准，以太阳脉冲作为图像扫描基准，太阳、地球、卫星三者之间的相对关系在连续不断地运动变化。

The FY-2 spin stabilized geosynchronous meteorological satellite uses the earth pulse for attitude control reference mark and uses the sun pulse for image scan reference mark .

这一准则不仅为陀螺仪设计提供理论依据，而且为飞行器用自旋稳定实现姿态控制提供理论依据。

The theoretical foundation of designing gyroscope and controlling the attitude of apace vehicle by using the spinning stability round its own axis may be based on the criteria .

FY2B是自旋稳定卫星，红外通道无法进行在轨星上绝对定标。

The FY 2B is a satellite with the spin stabilized attitude , it is had to make the absolute calibration for its IR channel while the satellite is in orbit .

小型月球探测器由地球停泊轨道向地月转移轨道射入时，要求采用自旋稳定来建立发动机的点火姿态。

Spin stability is taken for the small lunar explorer to build up the solid motor firing attitude when it was injected from the Earth berth orbit to the Earth Moon transfer orbit .

水平侧向力会导致自旋导弹不稳定飞行。

Horizontal side force may cause instability of spinning missile .

即当阻尼器参数确定后，双自旋卫星姿态稳定取决于平台和转子的标称角速度。

After damper parameter is given , the stability of dual spinning satellites will lie on angular velocity of the flat floor and rotor .

带挠性附件双自旋卫星的Liapunov稳定准则

Liapunov Stability Criteria for Dual Spin Satellites with Flexible Appendages

提出利用伺服系统设计技术改善自旋弹道导弹姿态稳定性能的思想。

The idea of attitude stability by servo system design is constructed .